Turbulence in a Shock-Wave Boundary-Layer Interaction-Reference-Cited by-同舟云学术

Turbulence in a Shock-Wave Boundary-Layer Interaction

Published:1975-07 Issue:7 Volume:13 Page:884-889
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Rose William C.¹,Johnson Dennis A.¹

Affiliation:

1. NASA Ames Research Center, Moffett Field, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.60464

Reference25 articles.

1. Shock-wave reflection from a turbulent boundary layer with mass bleed.

2. 4Grande, E. "An Investigation of the Unsteady Flow Properties of the Interaction Between a Shock Wave and a Turbulent Boundary Layer in Two-Dimensional Internal Flow," Ph.D. thesis,June 1971, Dept. of Aeronautics and Astronautics,Univ. of Washington, Seattle, Wash.

3. 5Rose, W.C. "The Behavior of a Compressible Turbulent Boundary Layer in a Shock-Wave Induced Adverse Pressure Gradient,", Ph.D. thesis,1972, Univ. of Washington, Seattle, Wash.; also TN 7092, March 1973, NASA.

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