USAAVLABS technical reports. 65-28. Effect of Mach number, Reynolds number and thickness ratio on aerodynamic characteristics of NACA 63A-series airfoil sections, Lockheed report LR 18596 [with bibliography]; by O. E. Sipe, jr. [and] N. B. Oorenberg.
Publication Title:
Effect of Mach number, Reynolds number and thickness ratio on aerodynamic characteristics of NACA 63A-series airfoil sections, Lockheed report LR 18596 [with bibliography]; by O. E. Sipe, jr. [and] N. B. Oorenberg.
Display Title:
USAAVLABS technical reports. 65-28. Effect of Mach number, Reynolds number and thickness ratio on aerodynamic characteristics of NACA 63A-series airfoil sections, Lockheed report LR 18596 [with bibliography]; by O. E. Sipe, jr. [and] N. B. Oorenberg.
Series Title:
USAAVLABS technical reports.
Corporate Agency Authors:
Transportation Corps (Army) and Defense Dept.
Sort Author:
Transportation Corps (Army)
Authors:
Sipe, O. E. jr. and Oorenberg, N. B.
Author place:
Washington, D.C.
Author zip:
20310
Date:
June 1965
Publish Date ISO Format:
1965-06-01T00:00:00Z
Publication Start:
19650601
Publication End:
19650630
Corporate/Agency Author:
Transportation Corps (Army)
Publication month:
7
Publication year:
1965
SuDoc number:
D 117.8/2:(nos.)
Description:
[1]+xii+464+[2] p. il. 4°
Notes:
(Task 1P128901A14203, contract DA 44-177-AMC-144(T).) [Prepared by Lockheed California Company, Burbank, Calif.] and (Army Aviation Materiel Laboratories, Fort Eustis, Va.) [Nos. 65-27 and 65-28 are designated USAAML technical reports.]
Notes:
(Army Aviation Materiel Laboratories, Fort Eustis, Va.) [Nos. 65-27 and 65-28 are designated USAAML technical reports.] Φ For Sale by OTS, Commerce Dept. (Price upon application.)
Availability:
Φ For Sale by OTS, Commerce Dept. (Price upon application.)