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
By: A. C. Browning, J. F. W. Crane and R. J. Monoghan.
Contributors: Crane, J. F. W.; Monoghan, R. J.; Royal Aircraft Establishment (Great Britain)
Series: Royal Aircraft Establishment. Technical note -- AERO. 2527
Publisher: Ministry of Supply, Royal Aircraft Establishment
Published: 1957
Place of publication: London
Number of pages: 25
Notes: Also published as : Aeronautical Research Council.

Current paper, no. 381.

Bibliography: p. 18-19.