Two-dimensional Wind-tunnel Investigation of the NACA 64(sub 1)-012 Airfoil Equipped with Two Types of Leading-edge Flap
1947-05-01
Sonstige
Keine Angabe
Englisch
AIRFOILS - NACA 641-012 - CHAR ,MOMENTS & ORDINATES , AIRFOILS - CHARACTERISTICS - EFFECT OF SURFACE ROUGHNESS , WINGS - HIGH LIFT DEVICES , WING FLAPS, LEADING-EDGE , WING FLAPS, SPLIT , WIND TUNNEL TESTS - NACA - PRESSURE, LOW-TURBULENCE (7 1/2 X 3') , WORK CARRIED ON AT LAL , LOW-DRAG (WING FLAPS)
Engineering Index Backfile | 1948
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