Ablation Onset in Unsteady Hypersonic Flow About Nose Tip with Cavity-Reference-Cited by-同舟云学术

Ablation Onset in Unsteady Hypersonic Flow About Nose Tip with Cavity

Published:2000-07 Issue:3 Volume:14 Page:421-434
ISSN:0887-8722
Container-title:Journal of Thermophysics and Heat Transfer
language:en
Short-container-title:Journal of Thermophysics and Heat Transfer

Author:

Silton Sidra I.¹,Goldstein David B.¹

Affiliation:

1. University of Texas at Austin, Austin, Texas 78712-1085

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

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.6540

Reference20 articles.

1. Engblom, W. A. “Numerical Investigation of Hypersonic Flow over a Forward-Facing Cavity,” Ph.D. Dissertation, Dept. of Aerospace Engineering and Engineering Mechanics,Univ. of Texas, Austin, TX,Aug. 1996, pp.20-29, 36, 41, 122-125, 128-143.

2. Yuceil, B. “An Experimental Investigation of a Forward-Facing Nose Cavity on a Blunt Body at Mach 5,” Ph.D. Dissertation, Dept. of Aerospace Engineering and Engineering Mechanics,Univ. of Texas, Austin, TX,Dec. 1995, pp.77-94, 123-132.

3. A preliminary investigation of the Helmholtz resonator concept for heat flux reduction

4. Experimental and numerical study of hypersonic forward-facing cavity flow

5. Fluid Dynamics of Hypersonic Forward-Facing Cavity Flow

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