Effects of wing elevation, incidence, and camber on the aerodynamic characteristics of a representative hypersonic cruise configuration at Mach numbers from 0.65 to 10.70
By: by Walter P. Nelms, Jr., and John A. Axelson.
Contributors: Axelson, John A., joint author.
Series: NASA technical note, NASA TN; D-6049
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: 73
Subjects: Aerodynamics, Hypersonic.; Airplanes -- Wings.
Notes: Bibliography: p. 9.
Cover title.