Computational Fluid Dynamics Prediction of Hyper-X Stage Separation Aerodynamics
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681-2199
2. FDC/NYMA, Inc., Hampton, Virginia 23681-2199
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3771
Reference27 articles.
1. Hyper-X stage separation - Background and status
2. Hyper-X Stage Separation Wind-Tunnel Test Program
3. Aerodynamic Database Development for the Hyper-X Airframe-Integrated Scramjet Propulsion Experiments
4. Integrated Aeropropulsive Computational Fluid Dynamics Methodology for the Hyper-X Flight Experiment
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