Application of supersonic linear theory and hypersonic impact methods to three nonslender hypersonic airplane concepts at mach numbers from 1.10 to 2.86
By: Jimmy L. Pittman
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA technical paper -- 1539
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1979
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 56
Subjects: Airplanes -- Mathematical models; Aerodynamics -- Mathematical models
Notes: "Langley Research Center."

"December 1979"--Cover

Subject Category 02

Includes bibliographical references