Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the Ames unitary plan wind tunnel
By: Paul M. Siemers, III,  Martin W. Henry.
Contributors: Henry, Martin W.; Langley Research Center.
Series: NASA technical memorandum -- 87654.
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 1986
Place of publication: Hampton, Va
Language: eng
Format: Microform
Subjects: Space shuttles.; Aerodynamic load.; Forebodies.; Models.; Orifices.; Pressure distribution.; Space shuttles.; Wind tunnel tests.
Notes: Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1986. 5 microfiches.