Results 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
A low-speed wind-tunnel investigation was made to determine the lateral control characteristics of a...
This report contains the results of a series of tests with three wing models. By changing the sectio...
Wind-tunnel data are presented on the rate of change of yawing moment with sideslip for tests of 9 c...
Wind tunnel tests haved been made at low speed to various small-scale models of swept-back, swept-fo...
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...
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...
Results of a low-speed wind-tunnel investigation to determine the effect of high-lift devices on the...
Results are presented, in graphical and tabular form, from a wind tunnel investigation of the lift, ...
Wind-tunnel tests of a simplified nacelle on a semispan wing having approximately 35 degrees of swee...
An investigation has been made at large scale of the characteristics of highly swept wings. Data wer...
This report describes preliminary wind tunnel tests on a model of a monoplane wing equipped with win...
These experiments were carried out to determine the aerodynamic characteristics of various triplanes...
This report presents the results of wind-tunnel tests made on three model wings having different siz...
The results presented in this note show the effect of twist and sweepback on the span load distribut...
A low-speed wind-tunnel investigation was made to determine the lateral control characteristics of a...
This report contains the results of a series of tests with three wing models. By changing the sectio...
Wind-tunnel data are presented on the rate of change of yawing moment with sideslip for tests of 9 c...
Wind tunnel tests haved been made at low speed to various small-scale models of swept-back, swept-fo...
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...
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...
Results of a low-speed wind-tunnel investigation to determine the effect of high-lift devices on the...
Results are presented, in graphical and tabular form, from a wind tunnel investigation of the lift, ...
Wind-tunnel tests of a simplified nacelle on a semispan wing having approximately 35 degrees of swee...
An investigation has been made at large scale of the characteristics of highly swept wings. Data wer...
This report describes preliminary wind tunnel tests on a model of a monoplane wing equipped with win...
These experiments were carried out to determine the aerodynamic characteristics of various triplanes...
This report presents the results of wind-tunnel tests made on three model wings having different siz...
The results presented in this note show the effect of twist and sweepback on the span load distribut...
A low-speed wind-tunnel investigation was made to determine the lateral control characteristics of a...
This report contains the results of a series of tests with three wing models. By changing the sectio...
Wind-tunnel data are presented on the rate of change of yawing moment with sideslip for tests of 9 c...
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