Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel
By: Theodore R. Creel, Jr., and Ivan E. Beckwith, Fang-Jenq Chen.
Contributors: Beckwith, Ivan E.; Chen, Fang-Jenq.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Series: NASA technical memorandum -- 86389.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1985
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Supersonic wind tunnels.; Reynolds number.; Boundary layer noise.
Notes: Cover title.

Distributed to depository libraries in microfiche.

STAR category 34.

Bibliography: p. 10.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1985. 1 microfiche ; 11 x 15 cm.