A theoretical and experimental study of the boundary layer flow on a 45 degree swept back wing
By: F. M. Burrows.
Contributors: College of Aeronautics (Cranfield, Bedfordshire)
Series: College of Aeronautics -- Cranfield. CoA Report ; no. 109
Publisher: College of Aeronautics
Published: 1956
Place of publication: Cranfield, Bedfordshire
Number of pages: 56
Notes: Bibliography: p. 41-44.