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Paper Citation Record · LEDGER

Lift augmentation by incorporating bend twist coupled composites in flapping wing

As of 13 August 2026, this Paper Citation Record lists 69 of 69 outbound references and 0 inbound Pith citation observations for arXiv:2505.23372.

A citation records a reference. It does not transfer a finding from one paper to another.

pith.paper-citation-record.v1
2505.23372 v1

Coverage vector

measured 69 of 69 reference resolution

Typed states for the displayed outbound observations.

Source: paper_references, paper_reference_links, observed 2026-08-07T12:51:50.084806Z

measured 69 of 69 standing notices

One-hop event checks from named stored sources.

Source: scholarly_work_events, retraction_status_cache, observed 2026-08-13T06:32:02.005865+00:00

measured 0 of 0 inbound itemization

Pith citing papers itemized under the disclosed page cap.

Source: paper_references, paper_reference_links

measured 0 of 1 external citation measurements

A source-named dated measurement, never combined with another source.

Source: cited_works

Reference resolution

69 of 69 outbound references displayed

  • verified exact8
  • verified fuzzy53
  • unresolved6
  • parse uncertain0
  • malformed identifier0
  • metadata mismatch2

External citation measurements

No source-named external measurement is stored.

Outbound references

Observation 94081338-5cb2-4769-836d-0987aa7793d0 · outbound

This paper cites Two dimensional mechanism for insect hovering,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Two dimensional mechanism for insect hovering,

Reference 1

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verified fuzzy
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Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

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Observation fbd90933-f8a0-43d0-8999-e9024d648bd8 · outbound

This paper cites Bumblebee flight in heavy turbulence,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Bumblebee flight in heavy turbulence,

Reference 2

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raw_fallback, observed 2026-08-07T12:52:38.367581Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:42.530855Z digest=sha256:d0667a294fa9f7c85bfb196c9639788f8d93a21600f9056bf85be9c01dc93532

Observation 6209d268-c7c2-430d-9984-d0485a1d47f2 · outbound

This paper cites Flapping wing flight can save aerodynamic power compared to steady flight,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Flapping wing flight can save aerodynamic power compared to steady flight,

Reference 3

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verified fuzzy
raw_fallback, observed 2026-08-07T12:52:38.157114Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:42.626323Z digest=sha256:cd2a399a613f141603927e3fbc287f8ef155fdd3a9c1540278a09d3ece7a3364

Observation ab483284-6b87-4034-8b82-711953c984e2 · outbound

This paper cites Collective flow enhancement by tandem flapping wings,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Collective flow enhancement by tandem flapping wings,

Reference 4

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verified fuzzy
raw_fallback, observed 2026-08-07T12:52:38.025831Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:42.702457Z digest=sha256:dc7a421258419841d57d0c4b148f5429cdcd2d545b034a580e99fde3687a1ad0

Observation 5c5430d6-5a82-4df6-93ac-839aba122c7c · outbound

This paper cites an unresolved cited work.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Unresolved cited work

Reference 5

Resolution
unresolved
raw_fallback, observed 2026-08-07T12:52:37.880462Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:42.820352Z digest=sha256:4d8e81672a25cd28ca381560c3ffad6bb4451639187a3d208edee714edc93516

Observation aafdfea6-7ac4-4cf0-b65b-a968cdd58dd6 · outbound

This paper cites Aerodynamic efficiency explains flapping strategies used by birds,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Aerodynamic efficiency explains flapping strategies used by birds,

Reference 6

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:37.680241Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:42.912994Z digest=sha256:f178c0bfa8e6ac09ef0cfe354ab2b7d6feb79f2a3491e085f2f7e92b1b59305a

Observation cb2c7858-09bf-4e36-ac8e-32a85bf6a5fc · outbound

This paper cites Wing kinematics of avian flight across speeds,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Wing kinematics of avian flight across speeds,

Reference 7

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:37.446012Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:43.025837Z digest=sha256:5ea4ce334c053b926ff7a37d275a288333d24957ba18a60f21e4acbb41f3939a

Observation 62caafba-c800-4e27-95d2-04d7746c067e · outbound

This paper cites Aerodynamic performance and flow mechanism of 3D flapping wing using discrete vo rtex method,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Aerodynamic performance and flow mechanism of 3D flapping wing using discrete vo rtex method,

Reference 8

Resolution
metadata mismatch
raw_fallback, observed 2026-08-07T12:51:52.519972Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:43.200591Z digest=sha256:eb37076318a5672f81269e255d0f13547a9380ec5ea93be13e4008b8435158ae

Observation 0f636f43-7f44-4746-a986-feb091775e62 · outbound

This paper cites Numerical simulations of bio -inspired approaches to enhance underwater swimming efficiency ,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Numerical simulations of bio -inspired approaches to enhance underwater swimming efficiency ,

Reference 9

Resolution
unresolved
no resolver link, observed 2026-08-07T12:51:43.392036Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

source=pdf_text observed=2026-08-07T12:51:43.392036Z digest=sha256:3273ea5247066db870bd83dd15317e8fad7794ff49bbc9bee30b354efa8224f8

Observation 88ac062e-409d-424f-a847-ad8350ac25af · outbound

This paper cites Vortex wake and flight kinematics of a swift in cruising flight in a wind tunnel,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Vortex wake and flight kinematics of a swift in cruising flight in a wind tunnel,

Reference 10

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:37.139978Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:43.574703Z digest=sha256:2d1012cde06b87495b0278a38469448f7c7558d7e0e8029e5c7fcbd4e47ab76d

Observation 29672e26-fe31-4544-905c-fd4d9b101889 · outbound

This paper cites Effects of flexibility on the aerodynamic performance of flapping wings,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Effects of flexibility on the aerodynamic performance of flapping wings,

Reference 11

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:36.815750Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:43.703182Z digest=sha256:7a48fac9745926fecfb72c12c985afcbce1a5fb25bcbf4ed2d6ace966e68e423

Observation c2370164-99a4-4e3b-ab5e-0ceba6760733 · outbound

This paper cites Optimization ‐ based study of bend –twist coupled rotor blades for passive and integrated passive/active load alleviation,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Optimization ‐ based study of bend –twist coupled rotor blades for passive and integrated passive/active load alleviation,

Reference 12

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:01.651615Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:43.814060Z digest=sha256:6ed93551d72888f4726ba49f5ae3f176eeee09e3d63b03006b1ff17b3536881a

Observation 6e673fb0-4926-438b-a692-09aa8a37159b · outbound

This paper cites Optimal Design of Wind Turbine Blades with Bend -Twist Couplings Effects,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Optimal Design of Wind Turbine Blades with Bend -Twist Couplings Effects,

Reference 13

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:01.527024Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:43.917241Z digest=sha256:a975f4a47789fe8dce9c941fd14d6bbc69f73729bd6607f1ac62a8ae19125589

Observation 8493bcd7-a17b-4e94-9828-f0678b1bf809 · outbound

This paper cites Numerical investigation of an insect -scale flexible wing with a small amplitude flapping kinematics,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Numerical investigation of an insect -scale flexible wing with a small amplitude flapping kinematics,

Reference 14

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:01.378100Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:44.022376Z digest=sha256:18bcc6b304d337ddb04ed0b5ccd748923f6d22425036e80ab179400d93d6ffcc

Observation 301f7683-db06-41a4-b19e-e2f538b33805 · outbound

This paper cites Aerodynamic technologies to improve aircraft performance,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Aerodynamic technologies to improve aircraft performance,

Reference 15

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:01.265150Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:44.147484Z digest=sha256:a9aaf90f69f0cea32b0c801b0bdb45e53b1e5f561e40271a5fe8cd3f500ba4d5

Observation e6912c8c-53b9-458e-bcb3-9cf08f024c9d · outbound

This paper cites On the role of vortical structures in aerodynamic performance of a hovering mosquito,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing On the role of vortical structures in aerodynamic performance of a hovering mosquito,

Reference 16

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:01.090704Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:44.253332Z digest=sha256:eae8526f5e5364b8127dd7d8d7ac71b43f9b37835374cd5b8935592687d20367

Observation 4d95ab42-266a-46c5-85af-5cd498462161 · outbound

This paper cites Aerodynamic interaction of bristled wing pairs in fling,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Aerodynamic interaction of bristled wing pairs in fling,

Reference 17

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:00.904261Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:44.358483Z digest=sha256:cf328ab979a0df254cf778131ae28f907061278d47ced1c6ed8773bc915e9fb8

Observation 38df10bc-a0d0-4add-91d3-846c58e54a32 · outbound

This paper cites Aerodynamic performance of a free - flying dragonfly—A span-resolved investigation,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Aerodynamic performance of a free - flying dragonfly—A span-resolved investigation,

Reference 18

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:00.731575Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:44.452050Z digest=sha256:f71f1cbb8969e8e466e10d6dbe92f691fd430a33f7e32e137e4677b0eb7b05d9

Observation f80dfd98-a1d9-4b3c-b681-d8ffde2a1553 · outbound

This paper cites The spatial -temporal effects of wing 19 flexibility on aerodynamic performance of the flapping wing,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing The spatial -temporal effects of wing 19 flexibility on aerodynamic performance of the flapping wing,

Reference 19

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:00.485451Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:44.546123Z digest=sha256:3a8e08525081880082c8a3144e9a4d02adc165f099f946c0b34220a16735ed81

Observation 9e45bfec-e14d-42e5-8be3-50a4423574a9 · outbound

This paper cites Extension -twist coupling optimization in composite rotor blades,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Extension -twist coupling optimization in composite rotor blades,

Reference 20

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:00.332982Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:44.673319Z digest=sha256:15be7d6acdca7bba8cf5af65c105dc9947cb228cd9241fc720c5e8fff5b8e934

Observation 7536b3c3-88cb-45c6-bcf0-5c679497010f · outbound

This paper cites Optimization of extension -twist coupled composite blades for high -speed rotorcraft,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Optimization of extension -twist coupled composite blades for high -speed rotorcraft,

Reference 21

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:00.166243Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:44.776872Z digest=sha256:cf7efc083d44ae19a0cd2392beb32b7b389b48bc892727d98be150e2b9162c16

Observation 88a5f178-816b-47a9-9a3a-0e96c7afb107 · outbound

This paper cites Non -linear aeroelastic prediction for aircraft applications,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Non -linear aeroelastic prediction for aircraft applications,

Reference 22

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verified fuzzy
raw_fallback, observed 2026-08-07T12:51:59.999545Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:44.880621Z digest=sha256:b7c8867c345b741e11f79f5625de2def8f5a356baa1ed496f86c2cbbc58fab85

Observation 2646af20-8520-4aec-b543-cad2ee70bba6 · outbound

This paper cites Advances in biomedical fluid –structure interaction: Methodologies and applications from an interfacing perspective,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Advances in biomedical fluid –structure interaction: Methodologies and applications from an interfacing perspective,

Reference 23

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:59.791408Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:44.999555Z digest=sha256:2f786c0302b9ed679f99d2c430b068a549b9ba2b4853c40dd31f6a4ea091ff15

Observation c8ab408b-16cf-4464-98e2-cdc7e2e136e9 · outbound

This paper cites Numerical investigation of structural geometric nonlinearity effect in high -aspect-ratio wing using CFD/CSD coupled approach,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Numerical investigation of structural geometric nonlinearity effect in high -aspect-ratio wing using CFD/CSD coupled approach,

Reference 24

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:59.641720Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:45.105143Z digest=sha256:96cc2cd82d8447f9c7450a51faaefc16113d1091ce225d8cc7a72b8f6fecc7fc

Observation 4f38b105-d3c8-47bc-b9b1-1a9b42e846fd · outbound

This paper cites Experimental and theoretical study on aeroelastic response of high-aspect-ratio wings,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Experimental and theoretical study on aeroelastic response of high-aspect-ratio wings,

Reference 25

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verified fuzzy
raw_fallback, observed 2026-08-07T12:51:59.435483Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:45.204901Z digest=sha256:8a0fc932a885f5002199e10e9feeea68eee23f3fc0c4607a304660c19b880e61

Observation 2c896ac4-a7eb-475c-a2e4-a7194872e9cc · outbound

This paper cites CFD -based analysis of nonlinear aeroelastic behavior of high -aspect ratio wings,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing CFD -based analysis of nonlinear aeroelastic behavior of high -aspect ratio wings,

Reference 26

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:59.224930Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:45.273479Z digest=sha256:393bf6c8832615704f55c4e31ef6f4da0d2dff0c8b94cb225a473a538dd11a50

Observation b4b8af94-041b-4fc3-813c-0a8cfa78c65f · outbound

This paper cites Numerical investigation of nonlinear aeroelastic effects on flexible high- aspect-ratio wings,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Numerical investigation of nonlinear aeroelastic effects on flexible high- aspect-ratio wings,

Reference 27

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:58.923081Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:45.349571Z digest=sha256:84d91c07235d57492d3b810f77c346220690e7579152dfcd58d181c6f7b12841

Observation 180f011e-38fe-4050-974f-10dab49fd730 · outbound

This paper cites Investigations on the effects of structural damping on vortex -induced vibration response of an airfoil at a high angle of attack via the aero-damping map,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Investigations on the effects of structural damping on vortex -induced vibration response of an airfoil at a high angle of attack via the aero-damping map,

Reference 28

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:58.757133Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:45.442657Z digest=sha256:20a4acbe5d0d7030c4616e1637bc6bf3a5fa77612d4c765a6ec882994adb5c25

Observation 6fe61089-5f67-4c1f-9bc3-6f4608a81f57 · outbound

This paper cites Fluid –structure interaction on vibrating square prisms considering interference effects,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Fluid –structure interaction on vibrating square prisms considering interference effects,

Reference 29

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:58.536704Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:45.538818Z digest=sha256:79fbea960633a2d7ebcaa925e30e14058225855a70be4e47f818f9281af5efc5

Observation 99d8a52a-4079-403f-ad4b-de8805079c05 · outbound

This paper cites Effect of wingtip bending morphing on gust-induced aerodynamics based on fluid-structure interaction method,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Effect of wingtip bending morphing on gust-induced aerodynamics based on fluid-structure interaction method,

Reference 30

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:58.370497Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:45.647170Z digest=sha256:14d9e2c8f4a8de77edac9accc6872cff24b34304ae21d8ab0c16b835d4c235f6

Observation cef6b48c-5c82-4460-b347-7b1ad26318f5 · outbound

This paper cites Unsteady flow control mechanisms of a bio - inspired flexible flap with the fluid –structure interaction,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Unsteady flow control mechanisms of a bio - inspired flexible flap with the fluid –structure interaction,

Reference 31

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:58.152555Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:45.756847Z digest=sha256:e10b79cd39e5449972306fbd1f0d230b8cccc74879156a90578c468593b80e25

Observation 7254eedd-977c-4f3c-b217-fcfb9e60f4a3 · outbound

This paper cites Wake -induced vibration of an elastic plate submerged in the wake of tandem circular cylinders,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Wake -induced vibration of an elastic plate submerged in the wake of tandem circular cylinders,

Reference 32

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:57.969547Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:45.830889Z digest=sha256:07a05fc9f8d4877e5ef4f506c905d6858ed6252c18d0a54d03240efd462e8712

Observation 46608fdb-47cd-4531-b523-f4a6494d1bfe · outbound

This paper cites Flow -induced response and wake characteristics of a flexible splitter plate attached to a circular cylinder in laminar flow,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Flow -induced response and wake characteristics of a flexible splitter plate attached to a circular cylinder in laminar flow,

Reference 33

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:57.768305Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:45.943988Z digest=sha256:98deac3a0f5ccf22a599265093497d095074910cdcc9bedbadc61aa641c4a8b5

Observation 0906b812-4dec-4fc7-9643-d8a3e2ae95c4 · outbound

This paper cites Bend -Twist Coupled Carbon -Fiber Laminate Beams: Fundamental Behavior and Applications,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Bend -Twist Coupled Carbon -Fiber Laminate Beams: Fundamental Behavior and Applications,

Reference 34

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:57.558661Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:46.071660Z digest=sha256:b66855e40f1db23164c95ad4c76bf112d0d57c44b0656168bd87568457388bf4

Observation d689c622-6e7d-4bfa-af82-6332e2011a3f · outbound

This paper cites Computationally efficient optimal design of hygrothermally stable laminate with bend –twist coupling by analytical and numerical strategy,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Computationally efficient optimal design of hygrothermally stable laminate with bend –twist coupling by analytical and numerical strategy,

Reference 35

Resolution
unresolved
no resolver link, observed 2026-08-07T12:51:46.208056Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

source=pdf_text observed=2026-08-07T12:51:46.208056Z digest=sha256:e374ce0875f0869672f5c19a74e303680f041ed78bd534322708c98368f227e4

Observation c4453fbc-84e9-4704-8cc4-43805cdd2b21 · outbound

This paper cites Effect of spanwise flexibility on flapping wing propulsion,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Effect of spanwise flexibility on flapping wing propulsion,

Reference 36

Resolution
verified exact
doi, observed 2026-08-07T12:51:51.801244Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:46.343266Z digest=sha256:762a70d9c7f87616d6231f71e4027686574a8900854df341e960ce91ade03d66

Observation 14a5425e-6ff7-4601-88de-d8e1ff5a2b33 · outbound

This paper cites High -fidelity aeroelastic computations of a flapping wing with spanwise flexibility,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing High -fidelity aeroelastic computations of a flapping wing with spanwise flexibility,

Reference 37

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:57.331414Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:46.435517Z digest=sha256:f685eccb1454c92f7752fb8a60584494e8f64c731fa82e10eb91d79451be2f41

Observation 2f5d5225-2ba0-451f-9a43-4dd8cfd44667 · outbound

This paper cites an unresolved cited work.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Unresolved cited work

Reference 38

Resolution
unresolved
raw_fallback, observed 2026-08-07T12:51:57.136136Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:46.549775Z digest=sha256:5bc55de9f8e764bb7a5f995c21d08d857400a606fb69333c1a0c3ba1a2e47e83

Observation 49fd7466-49ea-42a2-a54b-abd271c7bed8 · outbound

This paper cites A mixed -time-scale SGS model with fixed model-parameters for practical LES,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing A mixed -time-scale SGS model with fixed model-parameters for practical LES,

Reference 39

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:56.960614Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:46.673706Z digest=sha256:2b5e2272ea7f049fee4b07efec50434b2d2ed9a4db212456f38e1ea8268a1044

Observation 142276db-d8b5-43bb-ad02-6301f9932a68 · outbound

This paper cites Modelling the effect of freestream turbulence on dynamic stall of wind turbine blades,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Modelling the effect of freestream turbulence on dynamic stall of wind turbine blades,

Reference 40

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:56.746459Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:46.778306Z digest=sha256:783f9b2ac6931c106808d664c063b2d66581fca9056ed33799f9eef2b6c4aa67

Observation 35f482fc-002b-47bf-b926-885c73b0c633 · outbound

This paper cites Three - dimensional simulation for fast forward flight of a calliope hummingbird,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Three - dimensional simulation for fast forward flight of a calliope hummingbird,

Reference 41

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:56.581718Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:46.918622Z digest=sha256:2b66343da4cddf3dc1c1b7a3571c8f24dd5776c31c8dcd8428abaa3250f4c27e

Observation 88a904c0-3124-4a36-ab26-c57aac2c9f00 · outbound

This paper cites Aerodynamics of bird flight,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Aerodynamics of bird flight,

Reference 42

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:56.400456Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:47.031605Z digest=sha256:4dc6c4f0931b6c866b18189f0be2f339c60b8bae47e71678f9031d5ea6035483

Observation a86a3410-f8f9-4d92-a277-7e993982f549 · outbound

This paper cites ANSYS Fluent Theory Guide, Release 18.0. Ansys,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing ANSYS Fluent Theory Guide, Release 18.0. Ansys,

Reference 43

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:56.234921Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:47.136624Z digest=sha256:1eca6ddb844722241792f37ce9e28d1e39ac57454ae65f034470a76cc98c6ce3

Observation 13aa02c4-0e59-4c4d-bd43-5bd0a8251581 · outbound

This paper cites A fluid mechanicians view of wind engineering: Large eddy simulation of flow past a cubic obstacle,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing A fluid mechanicians view of wind engineering: Large eddy simulation of flow past a cubic obstacle,

Reference 44

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:56.095968Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:47.238560Z digest=sha256:706c299c59c77947c7c9b6426ae3b066f5a58de91d2dd6e58fa6593234a7f2f0

Observation 8adbf2ec-d75c-4b56-a8ae-6def88980213 · outbound

This paper cites ERCOFTAC/IAHR/COST workshop on refined flow modeling,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing ERCOFTAC/IAHR/COST workshop on refined flow modeling,

Reference 45

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:55.928825Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:47.356552Z digest=sha256:848f08c86e54c00616ae12dba25e5346aa1584340273467bc53d88678a91d06b

Observation 497f781a-c120-4368-9614-a8759657f933 · outbound

This paper cites Numerical simulation of flapping wing aerodynamic performance under gust wind conditions,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Numerical simulation of flapping wing aerodynamic performance under gust wind conditions,

Reference 46

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:55.744625Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:47.483388Z digest=sha256:98a15881241990d9a063cc3f021c6486b90aa1506cb05110b30379f68af79b3b

Observation 218d4f29-b027-459a-8f04-8c33c8584c33 · outbound

This paper cites Numerical simulation of bending and length -varying flapping wing using discrete vortex method,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Numerical simulation of bending and length -varying flapping wing using discrete vortex method,

Reference 47

Resolution
verified exact
doi, observed 2026-08-07T12:51:51.601844Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:47.565355Z digest=sha256:4c494e1a5d28aa58ab346c24745a9c38ea7185ddbea643e62e026f31fff5105d

Observation 116bb49b-71d0-47bc-85ef-4e0924804c11 · outbound

This paper cites Global optimization of actively morphing flapping wings,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Global optimization of actively morphing flapping wings,

Reference 48

Resolution
verified exact
doi, observed 2026-08-07T12:51:51.408312Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:47.674173Z digest=sha256:eb3ba252abe851008c865a7759b038b6002e9ce7a4510edc4a586fa4f5f505e4

Observation 3b7b843f-79da-45f4-8fc1-8cfbe340e901 · outbound

This paper cites Object -oriented unsteady vortex lattice method for flapping flight,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Object -oriented unsteady vortex lattice method for flapping flight,

Reference 49

Resolution
unresolved
no resolver link, observed 2026-08-07T12:51:47.803652Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

source=pdf_text observed=2026-08-07T12:51:47.803652Z digest=sha256:e4c55a79fceac302400aa7741dd7142b05564e8a1e79242e77b5592475314dff

Observation b3af665f-5fb6-4743-993d-229b05770a15 · outbound

This paper cites Lift and Thrust Characteristics of Flapping Wing Aerial Vehicle with Pitching and Flapping Motion,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Lift and Thrust Characteristics of Flapping Wing Aerial Vehicle with Pitching and Flapping Motion,

Reference 50

Resolution
metadata mismatch
raw_fallback, observed 2026-08-07T12:51:52.112818Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:47.919310Z digest=sha256:17527c29234400a3cd0ef67b023ddb1415b2e5a653d7821ef235026f57269acc

Observation e0e9902f-7f48-409f-a5cf-c36e59409276 · outbound

This paper cites Comparison of 2D finite element modeling assumptions with results from 3D analysis for composite skin - stiffener debonding,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Comparison of 2D finite element modeling assumptions with results from 3D analysis for composite skin - stiffener debonding,

Reference 51

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:55.523070Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:48.016309Z digest=sha256:55ea1cd8edc83ca9f0d756abfa485ca6e1673340fccee4452ce510aa51e49547

Observation a945eab1-1d2c-46a2-8c54-5a9915de5b9c · outbound

This paper cites Z., W., Gursul, I.: Effect of spanwise flexibility on flapping wing propulsion,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Z., W., Gursul, I.: Effect of spanwise flexibility on flapping wing propulsion,

Reference 52

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:55.330570Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:48.138642Z digest=sha256:aa18cb7375016aebaa6dd6ae1e14a61d3e59b000f2038b5123a6db481f5c58fa

Observation 6d19504d-452b-4b2e-b92a-51c066603d10 · outbound

This paper cites SDM 2013 student papers competition passive gust load alleviation through bend -twist coupling of composite beams on typical commercial airplane wings,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing SDM 2013 student papers competition passive gust load alleviation through bend -twist coupling of composite beams on typical commercial airplane wings,

Reference 53

Resolution
verified exact
doi, observed 2026-08-07T12:51:51.108968Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:48.251585Z digest=sha256:07f6b6f4e208e0b4b2d720fe0da15f91c589d9e79ca9580ed0894a894f6320e7

Observation 45feb459-d8d1-47f2-b7ed-e117f560407a · outbound

This paper cites A generalized von Mises criterion for yield and fracture,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing A generalized von Mises criterion for yield and fracture,

Reference 54

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:55.141992Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:48.361587Z digest=sha256:262d24dcc62ab550e6252538c1dab5edabab84f8fa47a7601ee334a74277cd45

Observation 726ff7eb-b376-4c03-8773-f85686f708a9 · outbound

This paper cites Stress Analysis of Composite Aircraft Wing using Coupled Fluid-Structural Analysis,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Stress Analysis of Composite Aircraft Wing using Coupled Fluid-Structural Analysis,

Reference 55

Resolution
verified exact
doi, observed 2026-08-07T12:51:50.877031Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:48.485442Z digest=sha256:b1956255fcd06721e25d12cd8badeecd2906e50655257b6853f46870aa07358e

Observation 6b29b74f-12cc-4fe3-bcc7-9e8304446eb3 · outbound

This paper cites Learning from bat: aerodyn amics of actively morphing wing,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Learning from bat: aerodyn amics of actively morphing wing,

Reference 56

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:54.948724Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:48.587682Z digest=sha256:0929e69ce5821e1d7eac2a4b9b347d547056a5932cd1d8a7cba02547a21ac9aa

Observation 0c988773-9e4a-4618-b8b5-6988b5cabc85 · outbound

This paper cites Unsteady aerodynamic model of flexible flapping wing,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Unsteady aerodynamic model of flexible flapping wing,

Reference 57

Resolution
verified exact
doi, observed 2026-08-07T12:51:50.714378Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:48.708999Z digest=sha256:b345a2702b4352aae0ef205df84f2f4a035efb0cd7e3e87ce88cabc5edbbe749

Observation 73c30a4a-5b7e-4c16-8be3-7eaf4068bd10 · outbound

This paper cites Vertebrate Flight, volume 27 de Zoophysiology.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Vertebrate Flight, volume 27 de Zoophysiology

Reference 58

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:54.737134Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:48.832646Z digest=sha256:f40dd4e61c5bed5163774cc5da2b904597e1eefbc7a53bec7b55f1830c9deb0c

Observation 9492a886-5c53-4ffa-8e97-e0eeb65e9cb6 · outbound

This paper cites Power requirements for horizontal flight in the pigeon Columba livia,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Power requirements for horizontal flight in the pigeon Columba livia,

Reference 59

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:54.530340Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:48.968022Z digest=sha256:022666c4652faab88c6f5c9a9ae37a8d65a048039106d3d98af6a7b87443c026

Observation 24544664-4f61-478b-a25e-819b50dd47d6 · outbound

This paper cites Unsteady airfoils,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Unsteady airfoils,

Reference 60

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:54.278992Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:49.062175Z digest=sha256:9a001f66c1042ca29939f148687c5a60b4517adc3dd47404c851ae13b3768777

Observation 9da63642-7e6c-46ef-bfb3-c226857bc9cb · outbound

This paper cites Experiments and numerical simulations on hovering three -dimensional flexible flapping wings,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Experiments and numerical simulations on hovering three -dimensional flexible flapping wings,

Reference 61

Resolution
verified exact
doi, observed 2026-08-07T12:51:50.555508Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:49.155897Z digest=sha256:0888e33392f6272a6a886a66df459760a402ee10699aba05cf30236aece564c3

Observation a5bf8074-5b3c-40cb-82ad-9a8e0385532b · outbound

This paper cites Effects of wing deformation on aerodynamic forces in hovering hoverflies,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Effects of wing deformation on aerodynamic forces in hovering hoverflies,

Reference 62

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:54.082877Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:49.302094Z digest=sha256:133251850edd39d3ad37b4694c736d8d3ebdc76a53c5e036b974d13b028f2c86

Observation 75522d18-8877-46df-8d72-b319616b07f1 · outbound

This paper cites Flight wing rotation and the aerodynamic basis of insect flight,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Flight wing rotation and the aerodynamic basis of insect flight,

Reference 63

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:53.857484Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:49.414021Z digest=sha256:5a59368a764a387ad9187d3be27bbc6aa21258dd69ae6c8a1fd90ffe9ee29831

Observation d988ea31-6375-443a-836a-1da1ef91bab7 · outbound

This paper cites Resonance of flexible flapping wings at low Reynolds number,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Resonance of flexible flapping wings at low Reynolds number,

Reference 64

Resolution
verified exact
doi, observed 2026-08-07T12:51:50.315071Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:49.522402Z digest=sha256:7bde5c9215daf031faf7c12c7a5ff2315dce05b32e6134f6c3fc1fd7e8ae080c

Observation 1bad4050-834f-44ea-b7a5-400a4aea1a1d · outbound

This paper cites Mechanisms for generating coherent packets of ha irpin vortices in channel flow,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Mechanisms for generating coherent packets of ha irpin vortices in channel flow,

Reference 65

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:53.602277Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:49.637409Z digest=sha256:a1091d70742a5d4195ef64fc522eb28a362db6348891e6638f3240cde301c29d

Observation 373df258-53b9-4274-a192-9a7175cf61a2 · outbound

This paper cites Eddies, streams, and convergence zones in turbulent flows,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Eddies, streams, and convergence zones in turbulent flows,

Reference 66

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:53.412387Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:49.745545Z digest=sha256:3b2489ecc560e3ab51779368dbbe06bbf85cedb4944f770701a0fbaed392060a

Observation 2b4de075-1316-4c78-8a29-1d27f9dc7992 · outbound

This paper cites Vortices behavior depending on the aspect ratio of an insect-like flapping wing in hover,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Vortices behavior depending on the aspect ratio of an insect-like flapping wing in hover,

Reference 67

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:53.142442Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:49.840500Z digest=sha256:eaa2fef10d1efebd74166f80ef9947152d4b393df00e60e8ee568763d2e70498

Observation 00333f6f-ead3-485a-82e0-cb09d64f87ae · outbound

This paper cites Can tip vortices enhance lift of a flapping wing?,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Can tip vortices enhance lift of a flapping wing?,

Reference 68

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:52.919044Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:49.958840Z digest=sha256:0c772f41bf4730c0365a090733c11ac6d39216c4d28049a160c936d1c0d24e15

Observation 1e457ecb-6343-4753-bdda-1e5a0242eeb3 · outbound

This paper cites an unresolved cited work.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Unresolved cited work

Reference 69

Resolution
unresolved
raw_fallback, observed 2026-08-07T12:51:52.747345Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-13T06:32:02.005865+00:00.

source=pdf_text observed=2026-08-07T12:51:50.084806Z digest=sha256:785ad318ecc3a27c9b40c2ab71b05c93a13e5e0ef5cb10b1007675da41c1707d

Pith citing papers

No inbound Pith citation observations are available.