Aerothermodynamic Shape Optimization of Hypersonic Entry Aeroshells-Reference-Cited by-同舟云学术

Aerothermodynamic Shape Optimization of Hypersonic Entry Aeroshells

Published:2010-06-26 Issue: Volume: Page:
ISSN:
Container-title:13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference
language:
Short-container-title:

Author:

Theisinger John¹,Braun Robert¹,Clark Ian¹

Affiliation:

1. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-9200

Reference11 articles.

1. Allen, H. J. and Eggers, A. J., Jr. "A Study of the Motion and Aerodynamic Heating of Ballistic Missiles Entering the Earth'sAtmosphereat HighSupersonicSpeeds," NACA TR-1381,1958.

2. Multi-Objective Hypersonic Entry Aeroshell Shape Optimization

3. Piegl,L.and Tiller,W.,The NURBS Book,2nded.,Springer-Verlag,Berlin,1997,pp.128-136.

4. Anderson,J.D.,Hypersonicand HighTemperature Gas Dynamics,2nd ed.,AIAAEducation Series,AIAA,Reston,VA,2006,pp.54-63,70-71,73-74,292,299-300,326-327,341-346.

Cited by 6 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. Aerothermodynamic Design Optimization of Hypersonic Vehicles;Journal of Thermophysics and Heat Transfer;2019-04

2. Aerothermodynamic Design Optimization of Hypersonic Vehicles;2018 Multidisciplinary Analysis and Optimization Conference;2018-06-24

3. An optimization-based procedure for self-generation of Re-entry Vehicles shape;Aerospace Science and Technology;2017-09

4. Effect of Fineness Ratio on Minimum-Drag Shapes in Hypersonic Flows;Journal of Spacecraft and Rockets;2014-05

5. Multi-Fidelity Approach to Estimate Heating for Three-Dimensional Hypersonic Aeroshells;Journal of Spacecraft and Rockets;2013-07