High-speed Tests of an Airfoil Section Cambered to Have Critical Mach Numbers Higher than Those Attainable with a Uniform-load Mean Line
1947-07-01
Sonstige
Keine Angabe
Englisch
WIND TUNNEL TESTS - AAL - HIGH-SPEED (3 1/2'X1') , AIRFOILS - NACA 66(109)-210 (A=1 0,CLI=0 6)- CHAR ,MOMENTS & (A=0 6,CLI=-0 4) , WORK CARRIED ON AT AAL , PRESSURE DISTRIBUTION - AIRFOILS - NACA 66(109)-210 , ORDINATES - LOW-DRAG , AIRFOILS - NACA 66-210 - CHAR & MOMENTS - LOW-DRAG , AIRFOILS, CAMBERED - CHARACTERISTICS - WIND TUNNEL TESTS , AIRFOILS - CHARACTERISTICS - EFFECT OF COMPRESSIBILITY
Engineering Index Backfile | 1947
|Engineering Index Backfile | 1948
|Engineering Index Backfile | 1949
|