Flight-Dynamics Instability Induced by Heat-Shield Ablation Lag Phenomenon-Reference-Cited by-同舟云学术

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Flight-Dynamics Instability Induced by Heat-Shield Ablation Lag Phenomenon

Published:2003-09 Issue:5 Volume:40 Page:615-621
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Lin T. C.¹,Sproul L. K.¹,Olmos M.¹,Thyson N. A.²

Affiliation:

1. TRW Systems, San Bernardino, California 92402

2. Textron Systems, Wilmington, Massachusetts 01864

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/2.6902

Reference13 articles.

1. Effect of ablation on the dynamics of spinning re-entry vehicles.

2. Effects of spin and mass addition on high-angle-of-attack re-entry

3. The influence of asymmetric transition on re-entry vehicle motion

Cited by 3 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. Flow Topology Around Gas, Liquid and Three-Dimensional Obstacles in Hypersonic Flow;AIAA Journal;2012-01

2. Flow Topology of Gas, Liquid and 3-D Obstacles in Hypersonic Flow;27th AIAA Applied Aerodynamics Conference;2009-06-14

3. Heat transfer analysis of charring ablators under aerodynamic heating;Aircraft Engineering and Aerospace Technology;2005-06-01

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