investigation at transonic speeds of the performance of various distributed roughness bands used to cause boundary-layer transition near the leading edge of a cropped Delta half-wing
By: E. W. E. Rogers and I. M. Hall.
Contributors: Hall, I. M.; Aeronautical Research Council (Great Britain)
Series: Aeronautical Reseach Council.  Current papers -- no. 481
Publisher: Ministry of Aviation, Aeronautical Research Council
Published: 1960
Place of publication: London
Notes: Bibliographical references: p. 8-9.