effect of tip bluntness on boundary-layer transition on a 15 degree included angle cone at M = 3.12 and 3.81
By: Ruth H. Rogers.
Contributors: Aeronautical Research Council (Great Britain)
Series: Aeronautical Research Council.  Current paper -- no. 598
Publisher: Aeronautical Research Council
Published: 1962
Place of publication: London, England
Number of pages: 22
Notes: Previously published as Royal Aircraft Establishment Tech.

Note No. Aero 2645- A.R.C. 21,695.

Bibliographical references: p. 13.