Design and testing of an axisymmetric flow nozzle for Mach number seven
By: K. R. Enkenhus and Norman B. Tucker.
Contributors: Tucker, Norman B.; UTIA
Series: UTIA technical note -- no. 4
Publisher: Institute of Aerophysics
Published: 1955
Place of publication: [Downsview, Ont.]
Number of pages: 27
Subjects: Hypersonic flow; Nozzles
Notes: Includes bibliographical references.