Ablation Modeling for Dynamic Simulation of Reentry Vehicles

Author:

Doman David1,Blake William1

Affiliation:

1. Air Force Research Laboratory/VACA

Publisher

American Institute of Aeronautics and Astronautics

Reference10 articles.

1. 1Noffz, G. K. and Bowman, M. P. "Design and Laboratory Validation of a Capacitive Sensor for Measuring the Recession of a Thin-Layered Ablator," Tech. Rep. NASA TM-4777, NASA Dryden Flight Research Center, Edwards, CA, 1996.

2. 5Dennis, D. and Cunningham, B. "Forces and Moments on Pointed and Blunt-Nosed Bodies of Revolution at Mach numbers from 2.75 to 5.00," Tech. Rep. RM A52E22, NACA, Aug. 1965.

Cited by 2 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. Incorporation of Ablative Shape Change into Conceptual Hypersonic Mission Design;AIAA Atmospheric Flight Mechanics Conference;2016-01-01

2. Rapid Modeling of Ablative Shape Change for Conceptual Hypersonic Mission Design;AIAA Atmospheric Flight Mechanics Conference;2015-01-02

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