Drag of rectangular cavities in supersonic and transonic flow including the effects of cavity resonance-Reference-Cited by-同舟云学术

Drag of rectangular cavities in supersonic and transonic flow including the effects of cavity resonance

Published:1970-11 Issue:11 Volume:8 Page:1959-1964
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

MCGREGOR O. WAYNE¹,WHITE ROBERT A.²

Affiliation:

1. Fort Worth Division of General Dynamics, Fort Worth, Tex.

2. University of Illinois, Urbana-Champaign, Urbana, III.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.6032

Reference20 articles.

1. An Investigation of Separated Flows - Part I: The Pressure Field

2. An Investigation of Separated Flows- Part I I : Flow in the Cavity and Heat Transfer

3. Golik, R. J. "On Dissipative Mechanisms within Separated Flow Regions (with Special Considerations to Energy Transfer across Turbulent Compressible Prt= 1, Mixing Regions)," Ph.D. thesis,1962, Dept. of Mechanical and Industrial Engineering,Univ. of Illinois, Urbana, 111.

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