Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camber
By: S. Naomi McMillin ... [et al.].
Contributors: McMillin, S. Naomi; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 4673
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1996
Place of publication: [Washington, D.C; Springfield, Va
Language: eng
Format: Microform
Subjects: Delta wings.; Flow visualization.; Leading edges.; Camber.; Pressure ratio.
Other titles: Surface pressure and flow visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading edge radius and camber
Notes: Shipping list no.: 98-0799-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 3 microfiches.