Wind tunnel test of Clark "Y", Clark "Y-15", Clark "Y-18", Clark "Y-21", Gottingen 398, and S.T.Ae.-27a, 6" x 36" airfoils, tests nos. 233, 234, and 237 (Airplane Section report).

Bibliographic Details

Corporate Author:	United States. Army. Air Corps
Format:	Government Document eBook
Language:	English
Published:	Washington : U.S. GPO, 1926.
Series:	Air Corps Info. Circ. Aviation No. 573 McCook Field Rpt. Serial No. 2700
Subjects:	Aerodynamics. Airplanes, Military. Electronic books.
Online Access:	Connect to the full text of this electronic document