Boundary layer measurements in the UTIA 5 - by 7 - inch supersonic wind tunnel
By: J. Ruptash.
Contributors: UTIA
Series: UTIA report no. 16
Publisher: Institute of Aerophysics
Published: 1952
Place of publication: [Downsview, Ont.]
Number of pages: 23
Subjects: Supersonic flow; Turbulent boundary layer
Notes: Includes bibliographical references.