Preliminary in-flight boundary layer transition measurements on a 45-degree swept wing at Mach numbers between 0.9 and 1.8
By: J. Blair Johnson.
Contributors: Dryden Flight Research Facility.
Series: NASA technical memorandum -- 100412
Publisher: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility
Published: 1988
Place of publication: Edwards, Calif
Language: eng
Format: Microform
Subjects: Laminar flow.
Notes: Distributed to depository libraries in microfiche.

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