Tables for the compressible flow of dry air
Subtitle: giving major parameters for the Mach number range 0 to 4 [gamma]=1.403
By: [by] E.L. Houghton and A.E. Brock.
Contributors: Brock, A. E. joint author.
Publisher: St. Martin's Press
Published: 1962
Place of publication: New York
Language: eng
Number of pages: 64
Subjects: Aerodynamics -- Tables.