Note on an application of the tilting plate method of Mach number variation for wind tunnel tests at low supersonic speeds
By: J. Seddon and L. Haverty.
Contributors: Haverty, L.; Aeronautical Research Council (Great Britain); Royal Aircraft Establishment (Great Britain)
Series: Royal Aircraft Establishment. Technical note -- no. Aero 2238; Aeronautical Research Council. Current papers -- no. 168
Publisher: Ministry of Supply, Aeronautical Research Council
Published: 1953
Place of publication: London
Notes: Cover date: 1954.

Bibliography: p. 7.