Wind tunnel test. Visual study of flow discontinuity on 6×13″, .15 cylindrical camber airfoil (report, of 14″ wind tunnel test no. 610), Airplane Section report; by E. N. Fales.
Publication Title:
Wind tunnel test. Visual study of flow discontinuity on 6×13″, .15 cylindrical camber airfoil (report, of 14″ wind tunnel test no. 610), Airplane Section report; by E. N. Fales.
Display Title:
Wind tunnel test. Visual study of flow discontinuity on 6×13″, .15 cylindrical camber airfoil (report, of 14″ wind tunnel test no. 610), Airplane Section report; by E. N. Fales.
Corporate Agency Authors:
Engineering Division, Air Service, and War Department
Sort Author:
Engineering Division
Authors:
Fales, E. N.
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 87.11/2:6/564
Description:
ii+22 p. il. 4°
Notes:
(Air Service. Air Service information circular, aviation, v. 6, no. 564, Apr. 24, 1926.)
Notes:
(Air Service. Air Service information circular, aviation, v. 6, no. 564, Apr. 24, 1926.) ‡ Official Use. Not Available.