Investigation of a mixed-compression axisymmetric inlet system at Mach numbers 0.6 to 3.5

An edition of Investigation of a mixed-compression axisymmetric inlet system at Mach numbers 0.6 to 3.5 (1970)

Investigation of a mixed-compression axisymmetric inlet system at Mach numbers 0.6 to 3.5

By Donald B. Smeltzer

0 (0 Ratings)

0 Want to read0 Currently reading0 Have read

Publish Date

1970

Publisher

National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.]

Language

eng

Pages

242

Description:

subjects: Air intakes, Airplanes, Supersonic Aerodynamics, Turbojet engines, Wind tunnels