An Evaluation of the Characteristics of a 10-percent-thick NACA 66-series Airfoil Section with a Special Mean-camber Line Designed to Produce a High Critical Mach Number
1948-07-01
Sonstige
Keine Angabe
Englisch
AIRFOILS - CHARACTERISTICS - EFFECT OF SURFACE ROUGHNESS , AIRFOILS - NACA 66-210 - CHAR & MOMENTS LOW-DRAG (WING FLAPS,SPLIT) PRESSURE D , AIRFOILS - NACA 66-210 (A=1 0,C1I=0 6) - CHAR , MOMENTS & ORDINATES (09) (A=0 6, , AIRFOILS - NACA 66(09)-210(1=1 0,C1I=0 6) - CHAR , MOMENTS & ORDINATES (A=0 6,C1