Hypersonic boundary-layer transition for X-33 phase II vehicle
By: R.A. Thompson ... [et al.].
Contributors: Thompson, R. A.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 207316
Publisher: American Institute of Aeronautics and Astronautics; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1998
Place of publication: Reston, Va; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Boundary layer transition.; Hypersonics.; Flow distribution.; Wind tunnel tests.; Finite volume method.; Flow visualization.
Other titles: Hypersonic boundary layer transition for X-33 phase 2 vehicle
Notes: Shipping list no.: 99-0199-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.