Add to ORKGTests showed the effect of the ailerons and the tip shapes on the general performance of the wing, as well as on the lateral control and stability characteristics. The hinge moments were not measured but the approximate values are given in the first report of the series
A flight investigation was conducted to determine the lateral-control characteristics of retractable...
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...
This investigation was carried out for the purpose of determining the effectiveness of ailerons and ...
This report covers the sixth of a series of investigations in which various lateral control devices ...
Tests were made with ordinary flap-type ailerons on two wings with different amounts of taper, one m...
This report is the fourth of a series on systematic tests conducted which compares lateral control d...
Discussed here are a series of systematic tests being conducted to compare different lateral control...
Three model wings, two with typical slotted ailerons and one with typical frise ailerons, have been ...
Results are given of a series of systemic tests comparing lateral control devices with particular re...
This report covers the twelfth of a series of tests conducted to compare different lateral control d...
This report covers the fifth of a series of systematic investigations in which lateral control devic...
This report presents the results of flight tests made to determine the lateral control characteristi...
Ailerons described in references 1, 2, and 3, are summarized in the form of empirical equations whic...
This report presents the results of wind tunnel tests to determine the effect of wing-tip shape and ...
A three-dimensional investigation of straight-sided-profile plain ailerons on a wing with 30 degrees...
A flight investigation was conducted to determine the lateral-control characteristics of retractable...
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...
This investigation was carried out for the purpose of determining the effectiveness of ailerons and ...
This report covers the sixth of a series of investigations in which various lateral control devices ...
Tests were made with ordinary flap-type ailerons on two wings with different amounts of taper, one m...
This report is the fourth of a series on systematic tests conducted which compares lateral control d...
Discussed here are a series of systematic tests being conducted to compare different lateral control...
Three model wings, two with typical slotted ailerons and one with typical frise ailerons, have been ...
Results are given of a series of systemic tests comparing lateral control devices with particular re...
This report covers the twelfth of a series of tests conducted to compare different lateral control d...
This report covers the fifth of a series of systematic investigations in which lateral control devic...
This report presents the results of flight tests made to determine the lateral control characteristi...
Ailerons described in references 1, 2, and 3, are summarized in the form of empirical equations whic...
This report presents the results of wind tunnel tests to determine the effect of wing-tip shape and ...
A three-dimensional investigation of straight-sided-profile plain ailerons on a wing with 30 degrees...
A flight investigation was conducted to determine the lateral-control characteristics of retractable...
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...
This investigation was carried out for the purpose of determining the effectiveness of ailerons and ...