Confined normal-shock/turbulent-boundary-layer interaction followed by an adverse pressure gradient-Reference-Cited by-同舟云学术

Confined normal-shock/turbulent-boundary-layer interaction followed by an adverse pressure gradient

Published:1989-01-09 Issue: Volume: Page:
ISSN:
Container-title:27th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

SAJBEN M.¹,MORRIS M.¹,BOGAR T.¹,KROUTIL J.¹

Affiliation:

1. McDonnell Douglas Research Laboratories, Saint Louis, MO

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1989-354

Reference43 articles.

1. 222-576 Fig. 2 Spark schlieren photograph of flowfield.

2. X ue 'JPtp -44.5 0.0 1.263 -38.1 7.7 1.269 -31.8 15.3 1.254 -25.4 23.0 1.252 -19.0 30.6 1.232 -12.7 38.3 1.170 -6.3 46.0 1.125 0.0 53.6 1.006 6.3 61.2 0.986 12.7 68.9 1.001 19.0 76.5 0.994 25.4 56.6 0.985 31.8 91.8 0.983 38.1 99.5 0.972 44.5 107.1 0.969 78.7 148.4 0.917 88.9 160.7 0.895 101.6 176.0 0.882 114.3 191.3 0.867 127.0 206.6 0.852 139.7 221.9 0.841 152.4 237.2 0.816 177.8 267.8 0.792 203.2 298.4 0.765 228.6 329.0 0.748

3. 88-222-628

4. =148.5 n x =330.2mm 2 =451.4

5. 88-222567 Fig. 6 Contour plots of U(z,y) at three different

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