Surface-pressure and flow-visualization data at mach number 1.60 for three 65p0s delta wings varying in leading-edge radius and camber
By: S. Naomi McMillin ... [et al.].
Contributors: McMillin, S. Naomi; Langley Research Center.
Series: NASA technical memorandum -- 4673
Publisher: National Aeronautics and Space Administration, Langley Research Center; Available from NASA Center for AeroSpace Information
Published: 1996
Place of publication: Hampton, Va; Linthicum Heights, Md
Language: eng
Number of pages: 262
Subjects: Aerodynamics, Supersonic.; Airplanes -- Wings, Triangular.; Camber (Aerofoils); Leading edges (Aerodynamics)
Other titles: Surface pressure and flow visualization data at mach number 1.60 for three 65. delta wings varying in leading edge radius and camber
Notes: "December 1996."

"Performing organization report number L-17443"--Report documentation page.

Includes bibliographical references.

Performed by Langley Research Center WU 505-59-53-05