High Reynolds number tests on a 70 degree L.E. sweepback delta wing and body (H.P. 100) in the compressed air tunnel
By: R. W. F. Gould and C. F. Cowdrey.
Contributors: Cowdrey, C. F.; Aeronautical Research Council (Great Britain)
Series: Aeronautical Research Council. Current papers -- no. 387
Publisher: Ministry of Supply, Aeronautical Research Council
Published: 1955
Place of publication: London
Notes: Cover date: 1958.

Bibliography: p. 6.