Numerical simulation of hypersonic flow over an aeroassist flight experiment vehicle
Author:
Affiliation:
1. NASA, Johnson Space Center; Lockheed Engineering and Management Services Co., Inc., Houston, TX
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1988-2675
Reference11 articles.
1. Enhancements to Program LAURA for computation of three-dimensional hypersonic flow
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Proposed radiometric measurement of the wake of a blunt aerobrake;Journal of Spacecraft and Rockets;1992-11
2. Aeroassist flight experiment heating-rate sensitivity study;Journal of Thermophysics and Heat Transfer;1991-10
3. Effect of electron temperature and impact ionization on Martian return AOTV flowfields;Journal of Thermophysics and Heat Transfer;1991-01
4. Upgrade of PARC2D to include real gas effects;28th Aerospace Sciences Meeting;1990-01-08
5. Calculation of convective heat transfer on highly blunt bodies at flow incidence;27th Aerospace Sciences Meeting;1989-01-09
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