A quiet tunnel investigation of hypersonic boundary-layer stability over a cooled, flared cone
Subtitle: final report
By: principal investigator, Gregory V. Selby ; submitted by the Old Dominion University Research Foundation.
Contributors: Old Dominion University. Research Foundation.; United States. National Aeronautics and Space Administration.
Series: [NASA contractor report] -- NASA CR-202200.
Publisher: Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1996
Place of publication: Norfolk, Va; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Adiabatic conditions.; Boundary layer stability.; Boundary layer transition.; Hypersonic flow.; Low noise.; Linear prediction.; Wind tunnel tests.; Wall temperature.; Aerodynamic noise.; Nose cones.; Nozzle walls.; Flow distribution.
Notes: Shipping list no.: 98-0983-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.