Measurements of the effect of surface cooling on boundary layer transition on a 15 degree cone. Part I: Tests at M=2 and 3 in an 8 in. x 9 in. wind tunnel at R.A.E./Bedford

Measurements of the effect of surface cooling ...
A. C. Browning, A. C. Browning
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Measurements of the effect of surface cooling on boundary layer transition on a 15 degree cone. Part I: Tests at M=2 and 3 in an 8 in. x 9 in. wind tunnel at R.A.E./Bedford

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Publish Date
Pages
25

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Book Details


Edition Notes

Also published as : Aeronautical Research Council.

Current paper, no. 381.

Bibliography: p. 18-19.

Published in
London
Series
Royal Aircraft Establishment. Technical note -- AERO. 2527

The Physical Object

Pagination
25 p. :
Number of pages
25

Edition Identifiers

Open Library
OL21498299M

Work Identifiers

Work ID
OL13397211W

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