Conceptual Modeling of Supersonic Retropropulsion Flow Interactions and Relationships to System Performance
Author:
Affiliation:
1. Guggenheim School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332
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.A32464
Reference20 articles.
1. Mars Exploration Entry, Descent, and Landing Challenges
2. Continuing Validation of Computational Fluid Dynamics for Supersonic Retropropulsion
3. Application of a Reynolds-Averaged Navier-Stokes Approach to Supersonic Retropropulsion Flowfields
4. Survey of Supersonic Retropropulsion Technology for Mars Entry, Descent, and Landing
5. The flow of a jet from a body opposing a supersonic free stream
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