Results of aerothermodynamic and boundary layer transition testing of 0.0362-Scale X-38 (Rev 3.1) vehicle in NASA Langley 20-inch Mach 6 tunnel
By: Scott A. Berry ... [et al.].
Contributors: Berry, Scott A.; Langley Research Center.
Series: NASA technical memorandum -- 112857.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1997
Place of publication: Hampton, Va; Springfield, VA
Language: eng
Format: Microform
Subjects: Boundary layer transition.; Aerodynamic heating.; Wind tunnel tests.; Angle of attack.; Reynolds number.; Aerothermodynamics.; Flow visualization.
Notes: Shipping list no.: 99-0055-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 2 microfiches.