Investigation of a mixed-compression axisymmetric inlet system at Mach numbers 0.6 to 3.5
By: by Donald B. Smeltzer and Norman E. Sorensen.
Contributors: Sorensen, Norman E., joint author.
Series: NASA technical note, NASA TN; D-6078
Publisher: National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.]
Published: 1970
Place of publication: Washington
Language: eng
Number of pages: 242
Subjects: Airplanes -- Turbojet engines -- Air intakes.; Aerodynamics, Supersonic.; Wind tunnels.
Notes: Includes bibliographical references.
Cover title.