An Investigation of the Section Characteristics of Plain Unsealed Ailerons on an NACA 66,1-115 Airfoil Section in the Langley 8-foot High-speed Tunnel
1949-01-01
Sonstige
Keine Angabe
Englisch
AIRFOILS - NACA 66,1-115 - CHAR , MOMENTS & ORDINATES - LOW-DRAG , PRESSURE DISTRIBUTION - AIRFOILS - NACA 66,1-115 , AILERONS, BEVELED , AILERONS - CHARACTERISTICS - EFFECT OF COMPRESSIBILITY , WIND TUNNEL TESTS - NACA - HIGH-SPEED (8') , PRESSURE DISTRIBUTION - AILERONS , AILERONS - HINGE MOMENTS , AILERONS - DEFLECTION
Engineering Index Backfile | 1949
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Engineering Index Backfile | 1941
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