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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
1957, Ministry of Supply, Royal Aircraft Establishment
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Book Details
Edition Notes
Also published as : Aeronautical Research Council.
Current paper, no. 381.
Bibliography: p. 18-19.
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December 11, 2009 | Created by WorkBot | add works page |