Upstream influence scaling of 2D and 3D shock/turbulent boundary layer interactions at compression corners

Author:

SETTLES G.1,PERKINS J.1,BOGDONOFF S.1

Affiliation:

1. Princeton University, Princeton, N.J.

Publisher

American Institute of Aeronautics and Astronautics

Reference52 articles.

1. Green' recognized this problem in 1970, stating that the available 2D experiments showed too great a disparity to serve as the basis of a correlation. In io years this situation has changed somewhat with the advent of new experiments. In particular, there are now a t least three highquality data 3ets availablelo-12 on the Re and 6 scaling of compression corner interactions for the same nominal flow conditions (equilibrium, adiabatic turbulent boundary layers at M ?r 3). r d

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