Scale-effect tests in a turbulent tunnel of the NACA 65 3-418, a
1.0 airfoil section with 0.20-airfoil-chord split flap
Wartime report ; L-128
1944
10 S., [9] Bl.
graph. Darst
Originally issued September 1944 as Advance restricted report L4I22
Report
English
The NACA full-scale wind tunnel
NTRS | 1934
|Engineering Index Backfile | 1944
|Full-Scale Tests of NACA Cowlings
NTRS | 1937
|Tests of NACA 0025 and 0035 airfoils in full-scale wind tunnel
Engineering Index Backfile | 1941
|