Distributions of velocity, enthalpy and shear stress in the compressible turbulent boundary layer on a flat plate
By: D. A. Spence.
Contributors: Royal Aircraft Establishment (Great Britain)
Series: Royal Aircraft Establishment.  Report no -- AERO.2631
Publisher: Ministry of Aviation
Published: 1959
Place of publication: London
Number of pages: 23
Notes: Bibliographical references: p. 22-23.