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.

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pith.paper-citation-record.v1
2507.09368 v1

Coverage vector

measured 35 of 35 reference resolution

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Source: paper_references, paper_reference_links, observed 2026-08-06T18:01:20.190488Z

measured 35 of 35 standing notices

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Reference resolution

35 of 35 outbound references displayed

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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

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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

Resolution: verified exact; doi, observed 2026-08-06T18:01:20.370361Z

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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

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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

Resolution: verified exact; doi, observed 2026-08-06T18:01:20.359996Z

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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

Resolution: verified exact; doi, observed 2026-08-06T18:01:20.350460Z

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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: verified exact; doi, observed 2026-08-06T18:01:20.341334Z

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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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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

Resolution: verified exact; doi, observed 2026-08-06T18:01:20.330447Z

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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

Resolution: verified exact; doi, observed 2026-08-06T18:01:20.321417Z

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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

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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: verified exact; doi, observed 2026-08-06T18:01:20.304881Z

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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

Resolution: verified exact; doi, observed 2026-08-06T18:01:20.296000Z

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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

Resolution: verified exact; doi, observed 2026-08-06T18:01:20.286795Z

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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

Resolution: verified fuzzy; raw_fallback, observed 2026-08-06T18:01:20.513876Z

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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

Resolution: verified exact; doi, observed 2026-08-06T18:01:20.277641Z

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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

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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: verified fuzzy; raw_fallback, observed 2026-08-06T18:01:20.496154Z

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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

Resolution: verified fuzzy; raw_fallback, observed 2026-08-06T18:01:20.487178Z

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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

Resolution: verified fuzzy; raw_fallback, observed 2026-08-06T18:01:20.477903Z

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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

Resolution: verified exact; doi, observed 2026-08-06T18:01:20.268406Z

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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

Resolution: verified exact; doi, observed 2026-08-06T18:01:20.257777Z

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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

Resolution: verified exact; doi, observed 2026-08-06T18:01:20.248892Z

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No event found in the named queried sources as of 2026-08-19T06:32:44.657259+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

Resolution: verified fuzzy; raw_fallback, observed 2026-08-06T18:01:20.469582Z

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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: verified exact; doi, observed 2026-08-06T18:01:20.239463Z

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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: verified fuzzy; raw_fallback, observed 2026-08-06T18:01:20.461268Z

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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

Resolution: verified fuzzy; raw_fallback, observed 2026-08-06T18:01:20.452484Z

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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

Resolution: verified fuzzy; raw_fallback, observed 2026-08-06T18:01:20.443707Z

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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

Resolution: verified fuzzy; raw_fallback, observed 2026-08-06T18:01:20.434961Z

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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

Resolution: verified fuzzy; raw_fallback, observed 2026-08-06T18:01:20.426445Z

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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

Resolution: verified fuzzy; raw_fallback, observed 2026-08-06T18:01:20.417580Z

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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

Resolution: verified fuzzy; raw_fallback, observed 2026-08-06T18:01:20.408733Z

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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

Resolution: verified exact; doi, observed 2026-08-06T18:01:20.230584Z

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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

Resolution: verified fuzzy; raw_fallback, observed 2026-08-06T18:01:20.400033Z

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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

Resolution: verified fuzzy; raw_fallback, observed 2026-08-06T18:01:20.390323Z

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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

Resolution: verified exact; doi, observed 2026-08-06T18:01:20.220574Z

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No event found in the named queried sources as of 2026-08-19T06:32:44.657259+00:00.

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