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, Alan Edward, joint author.
Edition: 2nd ed.
Publisher: Edward Arnold
Published: 1970
Place of publication: London
Language: eng
Number of pages: 64
Subjects: Aerodynamics -- Tables.