influence of high adverse pressure gradients on boundary layers in supersonic flow
By: John D. Lee.
Contributors: UTIA
Series: UTIA report no. 21
Publisher: Institute of Aerophysics
Published: 1952
Place of publication: [Downsview, Ont.]
Number of pages: 29
Subjects: Boundary layers; Pressure gradients; Supersonic flow
Notes: Includes bibliographical references.