Add to ORKGResults are presented of wind-tunnel tests made at low speed of various small-scale models of sweptback, sweptforward, and yawed wings. The tests covered changes in aspect ratio, taper ratio, and tip shape. Some data were obtained with high-lift devices on sweptback wings and with ailerons on sweptforward wings. The data have been briefly analyzed and some comparisons have been made with the available theory
Four N.A.C.A. 23012 wings were tested at several angles of yaw in the N.A.C.A. 7- by 10-foot wind tu...
Presented are the results of a low-speed wind tunnel test on a 5.33-aspect-ratio, semi-span wing wit...
Large scale wind tunnel investigation of low speed aerodynamic characteristics of supersonic transpo...
Wind tunnel tests haved been made at low speed to various small-scale models of swept-back, swept-fo...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
Results of a low-speed wind-tunnel investigation to determine the effect of high-lift devices on the...
A low scale wind tunnel investigation was conducted in rolling flow to determine the effects of aspe...
Results are presented of a wind-tunnel investigation made to determine the influence of the fuselage...
Wind-tunnel tests of a simplified nacelle on a semispan wing having approximately 35 degrees of swee...
A wind tunnel investigation was conducted in the Langley 12-Foot Low-Speed Wind Tunnel to study the ...
A wind-tunnel investigation was conducted in the Langley 12-Foot Low-Speed Tunnel to study the low-s...
Wind tunnel tests haved been made at low speed to various small-scale models of swept-back, swept-fo...
Measured values of lift, drag, and pitching moment at M(sub o) = 1.53 are presented for seven wings ...
Low speed wind tunnel testing of high aspect ratio variable sweep wing supersonic transport model fo...
Contains results of tunnel tests to determine effects of various combinations of split flaps, slats,...
Four N.A.C.A. 23012 wings were tested at several angles of yaw in the N.A.C.A. 7- by 10-foot wind tu...
Presented are the results of a low-speed wind tunnel test on a 5.33-aspect-ratio, semi-span wing wit...
Large scale wind tunnel investigation of low speed aerodynamic characteristics of supersonic transpo...
Wind tunnel tests haved been made at low speed to various small-scale models of swept-back, swept-fo...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
Results of a low-speed wind-tunnel investigation to determine the effect of high-lift devices on the...
A low scale wind tunnel investigation was conducted in rolling flow to determine the effects of aspe...
Results are presented of a wind-tunnel investigation made to determine the influence of the fuselage...
Wind-tunnel tests of a simplified nacelle on a semispan wing having approximately 35 degrees of swee...
A wind tunnel investigation was conducted in the Langley 12-Foot Low-Speed Wind Tunnel to study the ...
A wind-tunnel investigation was conducted in the Langley 12-Foot Low-Speed Tunnel to study the low-s...
Wind tunnel tests haved been made at low speed to various small-scale models of swept-back, swept-fo...
Measured values of lift, drag, and pitching moment at M(sub o) = 1.53 are presented for seven wings ...
Low speed wind tunnel testing of high aspect ratio variable sweep wing supersonic transport model fo...
Contains results of tunnel tests to determine effects of various combinations of split flaps, slats,...
Four N.A.C.A. 23012 wings were tested at several angles of yaw in the N.A.C.A. 7- by 10-foot wind tu...
Presented are the results of a low-speed wind tunnel test on a 5.33-aspect-ratio, semi-span wing wit...
Large scale wind tunnel investigation of low speed aerodynamic characteristics of supersonic transpo...