Experiments in supersonic turbulent flow with large distributed surface injection-Reference-Cited by-同舟云学术

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Experiments in supersonic turbulent flow with large distributed surface injection

Published:1968-01-22 Issue: Volume: Page:
ISSN:
Container-title:6th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

FERNANDEZ F.¹,ZUKOSKI E.¹

Affiliation:

1. CALIFORNIA INST. OF TECH., DANIEL AND FLORENCE GUGGENHEIM JET PROPULSION CENTER, PASADENA, CALIF.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1968-129

Reference9 articles.

1. Mugalev, V. P. "The Experimental Investication of the Subsonic Turbulent Boundary D La;cr on a Plate with hjcction, " Izvrsriii %;shikh Uchehrykh %:rvedcnii;Ayntloni.rval'c'nhnika, So. 3 1195Yr 3n. 72-79 (tr'anslated by.J. B. Gazley), R k d Corp. Report T-142 (Dec. 8, 1960). 5. Coles,D. F. "TheTurbulent Boundary Lay

Cited by 7 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. Control of cavity flow by upstream mass injection;22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference;1991-06-24

2. A computational model for thickening boundary layers with mass addition for hypersonic engine inlet testing;26th Joint Propulsion Conference;1990-07-16

3. Experimental study of hypersonic helium flow past sharp and blunt cones with large injection;Fluid Dynamics;1972-11

4. Experiments in supersonic turbulent flow with large distributed surface injection.;AIAA Journal;1969-09

5. Surface mass injection at supersonic and hypersonic speeds as a problem in turbulent mixing. I.;AIAA Journal;1969-04

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