Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel to determine the aerodynamic properties of tapered wings having partial-span flaps for high lift and ordinary ailerons for lateral control. Each of two Clark-y wings, tapered 5:1 and 5:3, was equipped with partial-span split flaps of two lengths and with ordinary ailerons extending from the outboard ends of the flap to the wing tips. Measurements of wing forces and moments and of aileron hinge moments were made for the two conditions of flaps neutral and deflected.
Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps
1937-01-01
Sonstige
Keine Angabe
Englisch
Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps
Engineering Index Backfile | 1937
|Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps
Engineering Index Backfile | 1937
|Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps
Engineering Index Backfile | 1937
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