High Reynolds number tests of the cast 10-2/DOA 2 airfoil in the Langley 0.3-meter transonic cryogenic tunnel - phase II
By: David A. Dress ... [et al.]
Contributors: Dress, David A; Langley Research Center
Series: NASA technical memorandum -- 86273
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 1984
Place of publication: Hampton, Va
Language: eng
Format: Microform
Subjects: Aerofoils; Reynolds number; Aerodynamics, Transonic; Transonic wind tunnels
Notes: "August 1984."

"N84-33382"--Microfiche header

Bibliography: p. 9

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1984. 4 microfiches ; 11 x 15 cm