An Experimental Investigation of an NACA 631-012 Airfoil Section with Leading-edge Suction Slots
01.08.1948
Sonstige
Keine Angabe
Englisch
BOUNDARY LAYER CONTROL - SUCTION - SLOTS , PRESSURE DISTRIBUTION - AIRFOILS - NACA 631-012 , WIND TUNNEL TESTS - AAL (10'X7')(WORK CARRIED ON AT AAL) , AIRFOILS - NACA 633-018 - LOW-DRAG , AIRFOILS - NACA 631-012 - CHAR , MOMENTS & ORDINATES , BOUNDARY LAYER CONTROL - AIRFOILS - NACA 631-012 , LOW-DRAG (WING SLOTS & FLAPS)
Experimental investigation of NACA 63-012 airfoil section with leading-edge suction slots
Engineering Index Backfile | 1948
|Engineering Index Backfile | 1950
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