Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges
By: Julio Chu and James M. Luckring.
Contributors: Luckring, James M.; Langley Research Center.
Series: NASA technical memorandum -- 4645.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1996
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Wind tunnel tests.; Delta wings.; Leading edges.; Reynolds number.; Mach number.; Vortices.; Slender wings.; Pressure distribution.; Subsonic speed.
Other titles: Small-radius leading edge.
Notes: Shipping list no.: 98-0799-M (v. 2).

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997- ] <1> microfiche.
Table of contents: title: v. 2. Small-radius leading edge.