Shape Optimization of Reentry Vehicles to Minimize Heat Loading-Reference-Cited by-同舟云学术

Shape Optimization of Reentry Vehicles to Minimize Heat Loading

Published:2019-07 Issue:3 Volume:33 Page:785-796
ISSN:0887-8722
Container-title:Journal of Thermophysics and Heat Transfer
language:en
Short-container-title:Journal of Thermophysics and Heat Transfer

Author:

Eyi Sinan¹,Hanquist Kyle M.¹,Boyd Iain D.¹

Affiliation:

1. University of Michigan, Ann Arbor, Michigan 48109

Funder

The Scientific and Technological Research Council of Turkey

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering

Reference33 articles.

1. AllenH. J. “The Aerodynamic Heating of Atmosphere Entry Vehicles:A Review,” NASA TM-X-54056, 1964.

2. Stagnation-point radiative heating relations for earth and Mars entries

3. AllenH. J.EggersA. J. “A Study of the Motion and Aerodynamic Heating of Ballistic Missiles Entering the Earth’s Atmosphere at High Supersonic Speed,” NACA TR-1381, 1958.

4. Optimum conical bodies for grazing hyperbolic entry.

5. SeiffA.TauberM. E. “Minimization of the Total Heat Input for Manned Vehicles Entering the Earth’s Atmosphere at Hyperbolic Speeds,” NASA TR-R-236, 1966.

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