Optimum conical bodies for grazing hyperbolic entry.
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.3385
Reference20 articles.
1. ATMOSPHERE ENTRY PROBLEMS OF MANNED INTERPLANETARY FLIGHT
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1. Shape Optimization of Reentry Vehicles to Minimize Heat Loading;Journal of Thermophysics and Heat Transfer;2019-07
2. Shape Optimization of Reentry Vehicles to Minimize Heat Loading;AIAA Scitech 2019 Forum;2019-01-06
3. Determination of the body shape for minimum radiative heating along a flight trajectory;Fluid Dynamics;1978
4. Hypersonic shapes of maximum drag for a given heat-transfer rate;Journal of Optimization Theory and Applications;1969-08
5. Entry Radiative Transfer;Re-entry and Planetary Entry Physics and Technology;1968
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