Investigation of NACA 64,2-432 and 64,3-440 Airfoil Sections with Boundary-layer Control and an Analytical Study of Their Possible Applications
1951-07-01
Miscellaneous
No indication
English
PRESSURE DISTRIBUTION - AIRFOILS - NACA 64,3-040 , AIRFOILS - NACA 64,3-440 (A=1 0)(MOD ) - CHAR & ORDINATES , BOUNDARY LAYER CONTROL - AIRFOILS - NACA 64,3-440 (A=1 0)(MOD ) , AIRFOILS - NACA 64,3-040 - ORDINATES , AIRFOILS - NACA 64,2-432 - CHAR & ORDINATES , PRESSURE DISTRIBUTION - AIRFOILS - NACA 64,2-032 , AIRFOILS - NACA 64,2-032 - ORDINATES , PRESSURE DISTRIBUTION - AIRFOILS - NACA 64,2-432 , BOUNDARY LAYER CONTROL - AIRFOILS - NACA 64,2-432 , PRESSURE DISTRIBUTION - AIRFOILS - NACA 64,3-440 (A=1 0)(MOD )
Boundary-layer and stalling characteristics of NACA 64A006 airfoil section
Engineering Index Backfile | 1949
|Tests of NACA 653-018 airfoil section with boundary-layer control by suction
Engineering Index Backfile | 1944
|Boundary-layer and stalling characteristics of NACA 64a010 airfoil section
Engineering Index Backfile | 1950
|