Mach 6 experimental and theoretical stability and performance of a finned cylindrical body at angles of attack up to 65 ̊
By: Edward R. Hartman and Patrick J. Johnston.
Contributors: Johnston, Patrick J.; Langley Research Center.
Series: NASA technical memorandum -- 89050.
Publisher: National Aeronautics and Space Administration, Langley Research Center; For sale by the National Technical Information Service
Published: 1987
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Guided missiles -- Stability.
Other titles: Mach six experimental and theoretical stability and performance of a finned cylindrical body at angles of attack up to 65 degrees.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1987. 1 microfiche.