Computational flow predictions for hypersonic drag devices
Author:
Affiliation:
1. Eloret Institute, Palo Alto, California 94303
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.25530
Reference20 articles.
1. PRESSURE AND HEAT TRANSFER ON HIGH-SPEED AERODYNAMIC DECELERATORS OF THE BALLUTE TYPE
2. A discussion of governing decelerator performance and design parameters in the supersonic flight regime
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