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Paper Citation Record · LEDGER

Lift augmentation by incorporating bend twist coupled composites in flapping wing

As of 14 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 2026-08-14T06:32:32.682623+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 2026-08-14T06:32:32.682623+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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:42.530855Z digest=sha256:761233a36cd394b022d70887f8e640eeff1540fc9ba96aae505d3f1b601142ed

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

Resolution
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 2026-08-14T06:32:32.682623+00:00.

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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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:42.702457Z digest=sha256:97a3ac497ddd6ea1a40272fcf40c8f0f9d2f647974cc7998a4215ace4d10aece

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:42.820352Z digest=sha256:ff19be0df71c4c3a57a51a2fc85bd4d85c284cfaab7e7363551ff88b350325f6

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:42.912994Z digest=sha256:7f42c8613ed504f137a77e738c70812014748f79e2dc7ca178cef7599bb60aa9

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:43.025837Z digest=sha256:efb6f7372a306d4c3ca600b0f8b5243bdff69dc5062981807fbf6da16ef338df

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:43.200591Z digest=sha256:41a7bcf3e644fe8916108a0542e04b6734aaf26bcab01c91149a917e3a1c7a77

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

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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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:43.574703Z digest=sha256:60eb91f96c0341016241ad4d6ba42ba9c2ef355c45aaeb82ee13b2cabe20b609

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:43.703182Z digest=sha256:cfb888c7fae18b38403e16274617c72684a6ff8127cc220c354d2f4f0a6bda30

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:43.814060Z digest=sha256:a820a3839efa3ccfb3824e4c2655a48959d995e69b98a3838731c421a3edf737

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:43.917241Z digest=sha256:232043573f20d724bd586dbf5ecba75ef1126ed930f0f018d6910659634924ef

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:44.022376Z digest=sha256:4a241f9037d289de284ca6857d7c30a9b451319641e190e3da343929a8327e02

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:44.147484Z digest=sha256:c365fa07c9b26280009d7deb2a09d8121f840d10a0fde16a19f2b7d5ced4daaf

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:44.253332Z digest=sha256:4d29a85cdf5ba35d22f015e3ea03c909b4682a2a26b4f7814765cefe4371f470

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:44.358483Z digest=sha256:364e65cfcb13a3b465e94c1c7b19a61a6fc65d512147d69f947b07845428e345

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:44.452050Z digest=sha256:a16a3b091d83a138d1738372876a4a7e86b2e7ee16192fefedeccd3dd67c23d4

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:44.546123Z digest=sha256:962ce89734d75911b0685a4f4aa993526d5e1382b6afd570530faba4c18daeee

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 2026-08-14T06:32:32.682623+00:00.

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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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:44.776872Z digest=sha256:b37c4a5fd5529f6c418aa97f5a16b5e22a4342ebb30a34947d539693609d1ec4

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:44.880621Z digest=sha256:76c05da63e6a59c08b485f827569a47028f819d84bbeec6904490ebd6f3336b3

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:44.999555Z digest=sha256:25984fede57431b61014a4e4cbac8ae8e1d0cd0cb8252e06dd8230ac5154d6a5

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:45.105143Z digest=sha256:230c7de15aa6b8a2ee3ec7b7380fa92a6dd39aee407e30dbc5a4bebf8914a5a8

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:45.204901Z digest=sha256:80d2219c07d45364031874d7712f25cd4d910bb1ac0e130b769eb2451448e532

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:45.273479Z digest=sha256:61dc0c05b2d0173ac2c9ff4e8894b158d5341ee8d6a378a70e33ce20eaad3cfc

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:45.349571Z digest=sha256:17c7f40447db67a93df307bec2f381eed3408b309e09212df083df3b9e47f52a

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:45.442657Z digest=sha256:94d00d75f80d764ddc17a8d53f690cc344730d8418aa563e870fb927e6eb6c95

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:45.538818Z digest=sha256:f33a2c08dc9e47f85e612698178d074b381cdefe102cfc185d2994f02be45509

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:45.647170Z digest=sha256:6ce23b21c8496f376da5a83e9cbeb36db1a7e673a1fac683a5cc133e4e060008

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:45.756847Z digest=sha256:e983cbe0f57ae72528558f4a419b6be5857daa6d1e5d199e96240da75719c3d6

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:45.830889Z digest=sha256:5b43883905c7d05852ca04e60199716d05f2aeedf97f3d4d8a7db73c9caa27cb

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:45.943988Z digest=sha256:e0bc685617f89f65014e49062f394c1b5425a230b6b4a2e0da5ffc151d708605

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

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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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:46.071660Z digest=sha256:8399a48142dc08bfd63292cf5f0242a5bdd79b63d7a84f62e398f6b156585005

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:46.343266Z digest=sha256:0d26c4ad0fb2457a28182f665e082c5f452d49986dcedf58446055d00cd845b9

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:46.435517Z digest=sha256:f66b1a2cb0c94a1ecb455190f4855b1ddf5ece4946a01b2dee4f70d3ea0faa61

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:46.549775Z digest=sha256:ba975359899312bf13654d33009c48f5c4542e3743059d04ea10268745d0bf2d

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:46.673706Z digest=sha256:00647df7b900551e4ae334e79157ccaba699e1e6445ad917b6f8e5c042557468

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:46.778306Z digest=sha256:490379ceb6f32de1896efd31303add27defb1eef929e6b61c05080df9d96c550

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:46.918622Z digest=sha256:dd2563155fb5c95188f4b16419e1e8741be518f4ce6e8a722d749c66c3539855

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:47.031605Z digest=sha256:e9b3bb724754d292967c098f7a4a875eba55ea037b3596bc7112c3f8276fe90a

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:47.136624Z digest=sha256:03f9eb5d0afcefac8fbce6807ffbd3c717aea919d67600212afbf458223e6448

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:47.238560Z digest=sha256:5e3936dda838317e2f9bbbb94cb64d5cec4cb940814680b1bf4b84c727b06e43

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:47.356552Z digest=sha256:8ae653f20dafccab01749785df3fd8cd26481ddfdf3426b53d404de91c7f0516

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:47.483388Z digest=sha256:8ff6eb1226cf67a2e24cedc22b56278d48536116da6a7d7673e781f4c0958546

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:47.565355Z digest=sha256:20b9e498b0dd233d00da517aa1e4872db29d8ec264a9b76b5c3f8792d81acd99

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:47.674173Z digest=sha256:cdae19828aefcb6e87f7f0f159b55e09d3d6a82955f0139a9a5ba88b372ed534

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:47.919310Z digest=sha256:b597dc15750d5c689f5685df3ab259cb578d8e77e66415e70416ae74a6392056

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:48.016309Z digest=sha256:38ce2084b58846f7f8af3a1f08b6571acd491e061994a49dc274c3928ceebfb0

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:48.138642Z digest=sha256:eed5f813542c1fb133ecd198126a458f0787f73ac1089837f856523074d78036

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:48.251585Z digest=sha256:600ab849aa54cd699606db4b594f085b1720045e1b70b1a75da2b37d49d4a067

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:48.361587Z digest=sha256:69ea8297e4eb0e6e55a79a53909eb09a5ecc7d508d334896bdfe203abb860531

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:48.485442Z digest=sha256:9914e11d1cba416cf666a8dc3262cbf46227e9fc23abda333ead8ccf69804154

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:48.587682Z digest=sha256:0c9999f27f0fb948f86619664e5fb9ac46a1bfb2dac2853677af61bc950aaa19

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:48.708999Z digest=sha256:f3e3b3b56e1353c946607ef78b6583bfb0434b2abab1a83083cfee5dbfdd56c9

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:48.832646Z digest=sha256:6a52c107d25a58479487e36ec6aeff77c70fcf3ab409c01e5c5e54b36df78baf

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:48.968022Z digest=sha256:f5f0fe8eeaaa4bb46157a506d3bfdaffa21eff139616946f8a065fc5345e0459

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:49.062175Z digest=sha256:6602f1deec3ec4cc27b36774623848ac8803c41196307713abf4cab5acc3f953

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:49.155897Z digest=sha256:142142661957656df6412d89c219589b6006c219698f3b4b2042a7460641620b

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:49.302094Z digest=sha256:045b4a0787536ec453f5f54e725e0caf1b0f3e6f685a9474222d6daf382113ae

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:49.414021Z digest=sha256:74428ab210f812256686d2efc6d742fbeabbb5307ce868448fefdde7e17f955a

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:49.522402Z digest=sha256:639a4a33fb0c0a98f3379d3a75b90796825ab64d5bf3e1fcd7b3c130234cbd56

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:49.637409Z digest=sha256:46296449f824076ce496bdaba7dad8961ce153b280027bd54057647885a413a1

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:49.745545Z digest=sha256:cac9bcbf9116024c7ab295c8a4536ec2a1d215afbd1594f6832d87ea3c23886e

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:49.840500Z digest=sha256:96fb541ad03f95804f9869d7f39d35e22d7e546244b51d7cb9907314b388ba10

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:49.958840Z digest=sha256:a9de64d7e1d8a3ec1c14974c7e354ab9de24b47f5770dccfb3a1a33a4fc5a893

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 2026-08-14T06:32:32.682623+00:00.

source=pdf_text observed=2026-08-07T12:51:50.084806Z digest=sha256:d2c33f7ac87c0f52c651d72e319c2738432f0c24980978827eae04a4d74311f9

Pith citing papers

No inbound Pith citation observations are available.