Wind tunnel test of Clark Y, Clark Y-15, Clark Y-18, Clark Y-21, Gottingen 398, and S. T. Ae'-27a, 6″X36″ airfoils, tests nos. 233, 234, and 237, Airplane Section report; prepared by Aerodynamics Branch.
Publication Title:
Wind tunnel test of Clark Y, Clark Y-15, Clark Y-18, Clark Y-21, Gottingen 398, and S. T. Ae'-27a, 6″X36″ airfoils, tests nos. 233, 234, and 237, Airplane Section report; prepared by Aerodynamics Branch.
Display Title:
Wind tunnel test of Clark Y, Clark Y-15, Clark Y-18, Clark Y-21, Gottingen 398, and S. T. Ae'-27a, 6″X36″ airfoils, tests nos. 233, 234, and 237, Airplane Section report; prepared by Aerodynamics Branch.
Corporate Agency Authors:
Engineering Division, Air Corps, and War Department
Sort Author:
Engineering Division
Date:
1926
Publish Date ISO Format:
1926-01-01T00:00:00Z
Publication Start:
19260101
Publication End:
19261231
Corporate/Agency Author:
Engineering Division
Publication month:
13
Publication year:
1926
SuDoc number:
W 87.11/2:6/573
Description:
ii+24 p. il. 4°
Notes:
(Air Corps. Air Corps information circular, aviation, v. 6, no. 573, Oct. 4, 1926.)
Notes:
(Air Corps. Air Corps information circular, aviation, v. 6, no. 573, Oct. 4, 1926.) ‡ Official Use. Not Available.