Tables for the compressible flow of dry air
Subtitle: giving major parameters for the Mach number range 0 to 4, [gamma]=1.403
By: E.L. Houghton and A.E. Brock.
Contributors: Brock, A. E.
Publisher: Arnold
Published: 1961
Place of publication: London
Language: eng
Number of pages: 64
Subjects: Aerodynamics -- Tables.