Effect of Reynolds number and Mach number on flow angularity probe sensitivity
By: Leigh Ann Smith and Jerry B. Adcock.
Contributors: Adcock, Jerry B.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Series: NASA technical memorandum -- 87750.
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, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Mach number.; Reynolds number.; Transonic wind tunnels.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington,D.C.? : National Aeronautics and Space Administration], 1986. 1 microfiche.