Effect of nose bluntness and afterbody shape on aerodynamic characteristics of a monoplanar missile concept with bodies of circular and elliptical cross sections at a mach number of 2.50
By: Ernald B. Graves and Roger H. Fournier
Contributors: Fournier, Roger H; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA technical memorandum -- 80055
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: 97
Subjects: Aerodynamics
Notes: "Langley Research Center."

"July 1979"--Cover

Subject category 02

Includes bibliographical references