The design and use of a temperature-compensated hot-film anemometer system for boundary-layer flow transition detection on supersonic aircraft
By: Harry R. Chiles.
Contributors: Dryden Flight Research Facility.
Series: NASA technical memorandum -- 100421.
Publisher: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility; For sale by the National Technical Information Service]
Published: 1988
Place of publication: Edwards, Calif; [Springfield, Va
Language: eng
Format: Microform
Subjects: Anemometer.; Aerospace telemetry.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1988. 1 microfiche.