Mach 6 flow field surveys beneath the forebody of an airbreathing missile
By: Patrick J. Johnston and James L. Hunt.
Contributors: Hunt, James L.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Series: NASA technical paper -- 2491.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service
Published: 1986
Place of publication: [Washington, D.C.]; Springfield, Va
Language: eng
Format: Microform
Subjects: Air breathing boosters.; Boundary layers.; Flow distribution.; Hypersonic speed.; Mach number.; Missiles.; Reynolds number.; Wind tunnel tests.
Notes: Includes bibliographical references.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1986] 2 microfiche.