Hot-Wall Reentry Testing in Hypersonic Impulse Facilities-Reference-Cited by-同舟云学术

Hot-Wall Reentry Testing in Hypersonic Impulse Facilities

Published:2013-02 Issue:2 Volume:51 Page:476-484
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Zander F.¹,Morgan R. G.¹,Sheikh U.¹,Buttsworth D. R.²,Teakle P. R.³

Affiliation:

1. School of Mechanical and Mining Engineering, University of Queensland, St Lucia, Queensland 4072, Australia

2. Computational Engineering and Science Research Centre, University of Southern Queensland, Toowoomba, Queensland 4350, Australia

3. Teakle Composites, Pinjarra Hills, Queensland 4069, Australia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J051867

Reference12 articles.

1. Ablation of Galileo Probe heat-shield models in a ballistic range

2. PLANETARY-ENTRY GAS DYNAMICS

3. LuF.MarrenD. (eds.) Advanced Hypersonic Test Facilities, Vol. 198, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2002, pp. 17–27.

4. MorganR. G. “Radiation Measurements in Simulated Ablation Layers,” Asian Office of Aerospace Research and Development Rept. AOARD-09-4144, 2010.

5. HuntD. C. “Measurement of Ablation in Transient Hypersonic Flow,” M.E.Sc. Thesis, Centre for Hypersonics, Univ. of Queensland, St Lucia, Queensland, Australia, 2001.

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