Boundary layer measurements in the UTIA 5 - by 7-inch supersonic wind tunnel
By: J. Ruptash.
Publisher: [Institute of Aerophysics]
Published: 1952
Place of publication: [Downsview, Ont.]
Number of pages: 23
Subjects: Supersonic flow; Turbulent boundary layer
Notes: Thesis (Ph.D.) - University of Toronto, 1952.

Includes bibliographical references.