Experimental surface pressure data obtained on 65̊ delta wing across Reynolds number and Mach number ranges

Experimental surface pressure data obtained on 65̊ delta wing across Reynolds number and Mach number ranges [microform] / Julio Chu and James M. Luckring.

Show other versions (1)
Saved in:
Bibliographic Details
Main Author: Chu, Julio
Corporate Author: Langley Research Center
Other Authors: Luckring, James M.
Other title:Small-radius leading edge.
Format: Government Document Microfilm Book
Language:English
Published: Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], [1996-]
Series:NASA technical memorandum ; 4645.
Subjects:
Wind tunnel > Examinations.
Airplanes > Wings, Triangular.
Reynolds number.
Mach number.
Aerodynamics.
Wind tunnel tests.
Delta wings.
Leading edges.
Vortices.
Slender wings.
Pressure distribution.
Subsonic speed.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number: NAS 1.15:4645
vol.2 Restricted Place a Hold

Similar Items