Nose-tip surface heat reduction mechanism-Reference-Cited by-同舟云学术

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Nose-tip surface heat reduction mechanism

Published:1996-01-15 Issue: Volume: Page:
ISSN:
Container-title:34th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Engblom W.¹,Goldstein D.¹

Affiliation:

1. Texas, Univ., Austin

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-354

Reference15 articles.

1. On a New Method for the Generation of Sound-Waves

2. Powell, A., and Smith, T.J. "Experiments ConcerningtheHartmannWhistle",Report 64-42,UCLA Dept.ofEngineering,Sep. 1964.

3. Burbank, P.B. and Stallings, R.L. "Heat^Transfer and Pressure Measurements on a Flat-Face Cylinder at a Mach Number Range of 2.49 to 4.44," NASATMX-221,1959.

Cited by 4 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. Nummerical Simulation in Influence of Forward-Facing Cavity on Aerodynamic Heating of Hypersonic Vehicle;Procedia Engineering;2012

2. A preliminary investigation of cold gas injection into a forward-facing cavity in hypersonic flow;35th Aerospace Sciences Meeting and Exhibit;1997-01-06

3. Fluid dynamics of hypersonic forward-facing cavity flow;34th Aerospace Sciences Meeting and Exhibit;1996-01-15

4. Heat Fluxes Inside a Cavity Placed at the Nose of a Projectile Measured in a Shock Tunnel at Mach 4.5;Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM)

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