Analysis of Navier–Stokes Codes Applied to Supersonic Retropropulsion Wind-Tunnel Test-Reference-Cited by-同舟云学术

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Analysis of Navier–Stokes Codes Applied to Supersonic Retropropulsion Wind-Tunnel Test

Published:2014-05 Issue:3 Volume:51 Page:680-692
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Zarchi Kerry A.¹,Schauerhamer Daniel G.²,Kleb William L.³,Carlson Jan-Renee³,Edquist Karl T.³

Affiliation:

1. Aerothermodynamics Branch, NASA Ames Research Center, Moffett Field, California 94035

2. Applied Aeroscience and Computational Fluid Dynamics Branch, Jacobs Technology, Inc., Houston, Texas 77058

3. Aerothermodynamics Branch, NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A32744

Reference39 articles.

1. Mars Exploration Entry, Descent, and Landing Challenges

2. High Mass Mars Entry, Descent, and Landing Architecture Assessment

3. ZangT. A.Dwyer-DiancioloA. M.KinneyD. J.HowardA. R.ChenG. T.IvanovM. C.SostaricR. R.WesthelleC. H. “Overview of the NASA Entry, Descent and Landing Systems Analysis Study,” AIAA Paper 2010-8649, Aug. 2010.

4. Performance Characterization of Supersonic Retropropulsion for High-Mass Mars Entry Systems

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1. Computational Modeling of Mars Retropropulsion Concepts in the Langley Unitary Plan Wind Tunnel;AIAA SCITECH 2022 Forum;2022-01-03

2. Status of Mars Retropropulsion Testing in the Langley Unitary Plan Wind Tunnel;AIAA SCITECH 2022 Forum;2022-01-03

3. Computational Analysis of a Multiple-Nozzle Supersonic Retropropulsion Configuration;AIAA AVIATION 2021 FORUM;2021-07-28

4. Similarity and Key Parameters of Retropropulsion Assisted Deceleration in Hypersonic Wind Tunnels;Journal of Spacecraft and Rockets;2021-07

5. Computational Investigation of Retropropulsion Operating Environments with a Massively Parallel Detached Eddy Simulation Approach;ASCEND 2020;2020-11-02

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