Heat transfer in a laminar boundary layer at Mach 2.5 from a surface having a temperature distribution
By: B. N. Pridmore-Brown.
Contributors: UTIA
Series: UTIA report -- no.45
Publisher: Institute of Aerophysics
Published: 1957
Place of publication: [Downsview, Ont.]
Number of pages: 19
Subjects: Aerodynamic heating; Heat transfer; Laminar boundary layer
Notes: Includes bibliographical references.