Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions
By: Y. Y. (Yat-Yung) Chan.
Contributors: UTIAS
Series: UTIAS report -- no.104
Publisher: Institute for Aerospace Studies
Published: 1965
Place of publication: [Downsview, Ont.]
Subjects: Axisymmetric flow; Compressible boundary layer; Hypersonic flow; Laminar boundary layer
Notes: Includes bibliographical references.