Typed states for the displayed outbound observations.
Source: paper_references, paper_reference_links, observed 2026-08-06T18:01:20.190488Z
Paper Citation Record · LEDGER
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone
As of 19 August 2026, this Paper Citation Record lists 35 of 35 outbound references and 0 inbound Pith citation observations for arXiv:2507.09368.
A citation records a reference. It does not transfer a finding from one paper to another.
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Source: scholarly_work_events, retraction_status_cache, observed 2026-08-18T06:34:40.430872+00:00
Pith citing papers itemized under the disclosed page cap.
Source: paper_references, paper_reference_links
A source-named dated measurement, never combined with another source.
Source: cited_works
Reference resolution
35 of 35 outbound references displayed
- verified exact17
- verified fuzzy16
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External citation measurements
No source-named external measurement is stored.
Outbound references
Observation 4c58176d-b4bd-4d97-8dbe-80e98a02b95f · outbound
This paper cites Hypersonic Laminar -Turbulent Transition on Circular Cones and Scramjet Forebodies.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Hypersonic Laminar -Turbulent Transition on Circular Cones and Scramjet Forebodies
Reference 1
- Resolution
- verified exact
- doi, observed 2026-08-06T18:01:20.380006Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation f8104064-f12d-4158-95fb-9c92a715834a · outbound
This paper cites Uncertainty Assessment of Hypersonic Aerothermodynamics Prediction Capability.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Uncertainty Assessment of Hypersonic Aerothermodynamics Prediction Capability
Reference 2
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- verified exact
- doi, observed 2026-08-06T18:01:20.370361Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation 6e3a26c6-10c4-44cb-bfff-93423ce543ad · outbound
This paper cites Surface Roughness Effects on the Hypersonic Flow Over Double -Wedge Bodies With a Blunt Leading Edge at Different Aft -Wedge Angles.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Surface Roughness Effects on the Hypersonic Flow Over Double -Wedge Bodies With a Blunt Leading Edge at Different Aft -Wedge Angles
Reference 3
- Resolution
- verified fuzzy
- raw_fallback, observed 2026-08-06T18:01:20.532047Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation 828088cd-7e83-4595-b39a-068dbb7d1f00 · outbound
This paper cites Finite-Rate Chemistry Effects in Turbulent Hypersonic Boundary Layers: A Direct Numerical Simulation Study.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Finite-Rate Chemistry Effects in Turbulent Hypersonic Boundary Layers: A Direct Numerical Simulation Study
Reference 4
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- doi, observed 2026-08-06T18:01:20.359996Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation 67eab497-5287-4b33-a791-80b382749df8 · outbound
This paper cites Coupled Flow, Thermal, and Structural Analysis of Aerodynamically Heated Panels.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Coupled Flow, Thermal, and Structural Analysis of Aerodynamically Heated Panels
Reference 5
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- verified exact
- doi, observed 2026-08-06T18:01:20.350460Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation 48b80910-f477-4f38-b696-1cdc4935eabd · outbound
This paper cites Aerothermoelastic Analysis of a Hypersonic Vehicle Based on Thermal Modal Reconstruction.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Aerothermoelastic Analysis of a Hypersonic Vehicle Based on Thermal Modal Reconstruction
Reference 6
- Resolution
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- doi, observed 2026-08-06T18:01:20.341334Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation eb646fef-2aa1-41d7-9593-c6bbdc0807e1 · outbound
This paper cites Roughness -Induced Transient Growth on a Hypersonic Blunt Cone.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Roughness -Induced Transient Growth on a Hypersonic Blunt Cone
Reference 7
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- raw_fallback, observed 2026-08-06T18:01:20.522568Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation ff8a856e-183e-44fe-8dcf-3ee3ba3e4b49 · outbound
This paper cites Effects of Roughness on Hypersonic Boundary-Layer Transition.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Effects of Roughness on Hypersonic Boundary-Layer Transition
Reference 8
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- doi, observed 2026-08-06T18:01:20.330447Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation 13b91210-185f-4dbc-bdcb-34b0dfed38f0 · outbound
This paper cites Nosetip Bluntness Effects on Cone Frustum Boundary Layer Transition in Hypersonic Flow.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Nosetip Bluntness Effects on Cone Frustum Boundary Layer Transition in Hypersonic Flow
Reference 9
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- doi, observed 2026-08-06T18:01:20.321417Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation f716617d-c17c-47b2-8072-8d3ea33f629d · outbound
This paper cites Theory of Stagnation Point Heat Transfer in Dissociated Air.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Theory of Stagnation Point Heat Transfer in Dissociated Air
Reference 10
- Resolution
- unresolved
- no resolver link, observed 2026-08-06T18:01:20.121564Z
Source-reported events for the cited work
Unavailable: canonical work link unavailable.
Observation 7c3d4099-fcec-4767-8b36-93141904561e · outbound
This paper cites Improved Fay-Riddell Procedure to Compute the Stagnation Point Heat Flux.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Improved Fay-Riddell Procedure to Compute the Stagnation Point Heat Flux
Reference 11
- Resolution
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- doi, observed 2026-08-06T18:01:20.304881Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation aa497862-b584-4cf5-ae15-b35999ce1d56 · outbound
This paper cites Computational Investigation and Simulation of the Aerothermodynamics of Reentry Vehicles.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Computational Investigation and Simulation of the Aerothermodynamics of Reentry Vehicles
Reference 12
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- doi, observed 2026-08-06T18:01:20.296000Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation a798df31-e5a1-4d20-9c09-daf7410f9084 · outbound
This paper cites Boundary -Layer Stability Analysis for Stetson’s Mach 6 Blunt -Cone Experiments.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Boundary -Layer Stability Analysis for Stetson’s Mach 6 Blunt -Cone Experiments
Reference 13
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- doi, observed 2026-08-06T18:01:20.286795Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation 23117e2d-ee68-417f-8bb3-415376b57dda · outbound
This paper cites Two -Temperature Extension of the HTR Solver for Hypersonic Turbulent Flows in Thermochemical Nonequilibrium.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Two -Temperature Extension of the HTR Solver for Hypersonic Turbulent Flows in Thermochemical Nonequilibrium
Reference 14
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- raw_fallback, observed 2026-08-06T18:01:20.513876Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation e2b2495b-fd1a-4c95-8c9e-925188d654bd · outbound
This paper cites V.; Subbareddy, P.K.; Brock, J.M.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone V.; Subbareddy, P.K.; Brock, J.M
Reference 15
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- doi, observed 2026-08-06T18:01:20.277641Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation 148725c7-6324-498e-9184-9de1e50dc181 · outbound
This paper cites an unresolved cited work.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Unresolved cited work
Reference 16
- Resolution
- unresolved
- raw_fallback, observed 2026-08-06T18:01:20.504856Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation 17f3c126-b040-424c-818a-6676283f4819 · outbound
This paper cites Nonequilibrium Gas Dynamics and Molecular Simulation; 2017; ISBN 9781139683494.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Nonequilibrium Gas Dynamics and Molecular Simulation; 2017; ISBN 9781139683494
Reference 17
- Resolution
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- raw_fallback, observed 2026-08-06T18:01:20.496154Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation d16e2f2f-46cf-48df-97ea-d93c065a71c0 · outbound
This paper cites Conservation Equations and Physical Models for Hypersonic Air Flows in Thermal and Chemical Nonequilibrium.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Conservation Equations and Physical Models for Hypersonic Air Flows in Thermal and Chemical Nonequilibrium
Reference 18
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- raw_fallback, observed 2026-08-06T18:01:20.487178Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation 01293d08-cb37-4aaf-bce4-f5895f13ccf6 · outbound
This paper cites Nonequilibrium Hypersonic Aerothermodynamics.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Nonequilibrium Hypersonic Aerothermodynamics
Reference 19
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Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation cdadc498-d985-47e5-adfd-91563e095411 · outbound
This paper cites Computational Aerothermodynamic Design Issues for Hypersonic Vehicles.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Computational Aerothermodynamic Design Issues for Hypersonic Vehicles
Reference 20
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- doi, observed 2026-08-06T18:01:20.268406Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation 254e5aec-1028-4b4f-aa6c-8ade21a1fabd · outbound
This paper cites Effect of Leading Edge Bluntness on Aerothermal Characteristics of Osculating Cone Waveriders.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Effect of Leading Edge Bluntness on Aerothermal Characteristics of Osculating Cone Waveriders
Reference 21
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- doi, observed 2026-08-06T18:01:20.257777Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation 1db38e06-0488-44da-b394-600c78e1521d · outbound
This paper cites Review of Testing Methods to Inform Materials Selection in High-Temperature Structural Applications.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Review of Testing Methods to Inform Materials Selection in High-Temperature Structural Applications
Reference 22
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- doi, observed 2026-08-06T18:01:20.248892Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation 8408dc50-29ab-42eb-85ee-94e7c2e0b3ef · outbound
This paper cites A CFD Validation Roadmap Hypersonic Flows.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone A CFD Validation Roadmap Hypersonic Flows
Reference 23
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- raw_fallback, observed 2026-08-06T18:01:20.469582Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation 7052592e-0cbd-4cbe-b69a-553186b32929 · outbound
This paper cites Distributed Roughness Effects on Blunt -Body Transition and Turbulent Heating.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Distributed Roughness Effects on Blunt -Body Transition and Turbulent Heating
Reference 24
- Resolution
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- doi, observed 2026-08-06T18:01:20.239463Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation 0a078eba-cda0-4a4a-a0af-7fbe72eaa079 · outbound
This paper cites On the Effects of Surface Roughness on Boundary Layer Transition.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone On the Effects of Surface Roughness on Boundary Layer Transition
Reference 25
- Resolution
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- raw_fallback, observed 2026-08-06T18:01:20.461268Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation e10842d8-e92b-4600-9bcc-dc814552c281 · outbound
This paper cites Computational Investigation of Roughness Effects on Boundary Layer Transition for Stetson’s Blunt Cone at Mach 6.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Computational Investigation of Roughness Effects on Boundary Layer Transition for Stetson’s Blunt Cone at Mach 6
Reference 26
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- raw_fallback, observed 2026-08-06T18:01:20.452484Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation dd85979e-fa61-4e6f-970b-3aa3e45e2330 · outbound
This paper cites Validation of CFD Simulations for Hypersonic Flow Over a Yawed Validation of CFD Simulations for Hypersonic Flow Over a Yawed Cone Cone.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Validation of CFD Simulations for Hypersonic Flow Over a Yawed Validation of CFD Simulations for Hypersonic Flow Over a Yawed Cone Cone
Reference 27
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- raw_fallback, observed 2026-08-06T18:01:20.443707Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation c9ffb293-5598-40b3-a802-91f746473411 · outbound
This paper cites The Finite Volume Method.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone The Finite Volume Method
Reference 28
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- raw_fallback, observed 2026-08-06T18:01:20.434961Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation 1741e083-f4d2-4cc4-b36a-aa49c29e0c62 · outbound
This paper cites An Introduction to Computational Fluid Dynamics: The Finite Volume Method.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone An Introduction to Computational Fluid Dynamics: The Finite Volume Method
Reference 29
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No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation 1b854e9a-df05-417b-9198-507c46968a52 · outbound
This paper cites Viscous Fluid Flow; McGraw-Hill New York, 2006; Vol.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Viscous Fluid Flow; McGraw-Hill New York, 2006; Vol
Reference 30
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- raw_fallback, observed 2026-08-06T18:01:20.417580Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation cf28a858-86c4-477e-8aa4-90815c1a8ca2 · outbound
This paper cites Momentum Transfer in Boundary Layers.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Momentum Transfer in Boundary Layers
Reference 31
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- raw_fallback, observed 2026-08-06T18:01:20.408733Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation c011270b-0d6f-42a3-b8b9-4fc25ef4b9c3 · outbound
This paper cites Causal Inference Analysis to Find Relationships Found in Boundarylayer Transition Part i: Theoretical.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Causal Inference Analysis to Find Relationships Found in Boundarylayer Transition Part i: Theoretical
Reference 32
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- doi, observed 2026-08-06T18:01:20.230584Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation caa941e7-3a39-4234-9110-f93d4fd19d6e · outbound
This paper cites Predicting Boundary-Layer Transition (BLT) Using Artificial Intelligence (AI) Causality Inference.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone Predicting Boundary-Layer Transition (BLT) Using Artificial Intelligence (AI) Causality Inference
Reference 33
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- raw_fallback, observed 2026-08-06T18:01:20.400033Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation 83ba09f5-2dd6-4ddf-9d59-5f457fbb0db5 · outbound
This paper cites The Near-Wall Mechanics of Three -Dimensional Turbulent Boundary Layers ; Stanford University, 1992; ISBN 9798208712337.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone The Near-Wall Mechanics of Three -Dimensional Turbulent Boundary Layers ; Stanford University, 1992; ISBN 9798208712337
Reference 34
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- raw_fallback, observed 2026-08-06T18:01:20.390323Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Observation b8cd6b5a-9b7b-4d13-b31f-325077d73da0 · outbound
This paper cites High -Reynolds-Number Fractal Signature of Nascent Turbulence during Transition.
Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone High -Reynolds-Number Fractal Signature of Nascent Turbulence during Transition
Reference 35
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- doi, observed 2026-08-06T18:01:20.220574Z
Source-reported events for the cited work
No event found in the named queried sources as of 2026-08-18T06:34:40.430872+00:00.
Pith citing papers
No inbound Pith citation observations are available.