Test of NACA 66,2-116, a = 0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the XP-63 airplane
1942-05-01
Sonstige
Keine Angabe
Englisch
WINGS - BELL P-63 WIND TUNNEL TESTS (NACA - 2-DIM PRESSURE) , WING FLAPS, BALANCED , WING FLAPS - HINGE MOMENTS , WIND TUNNEL TESTS - NACA - PRESSURE, LOW-TURBULENCE (7 1/2' X 3') , WING FLAPS, SLOTTED , AIRFOILS - NACA 66,2-116 - CHAR & MOMENTS LOW-DRAG (WING FLAPS, BALANCED & SLOT , PRESSURE DISTRIBUTION - WING FLAPS
Airfoil fitted with slotted flap
Engineering Index Backfile | 1936
|Wind-tunnel investigation of NACA 23021 airfoil with two sizes of balanced split flaps
Engineering Index Backfile | 1941
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