Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds
By: Patsy S. Fulton.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 101531.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1988
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 115
Subjects: Guided missiles -- Aerodynamics.; Angle of attack.; Euler equations of motion.; Missile configurations.; Pressure distribution.; Supersonic flow.; Transonic flow.; Wind tunnel models.; Wind tunnel tests.
Notes: Cover title.

Distributed to depository libraries in microfiche.

"November 1988."

Includes bibliographical references (p. 23).

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1988] 2 microfiches : negative.