Add to ORKGThis report covers the twelfth of a series of tests conducted to compare different lateral control devices with particular reference to their effectiveness at high angles of attack. The present wind tunnel tests were made with two sizes of upper-surface ailerons on rectangular Clark Y wing models equipped with full span split flaps. The tests showed the effect of the upper-surface ailerons and of the split flaps on the general performance characteristics of the wings, and on the lateral controllability and stability characteristics. The results are compared with those for plain wings with ordinary ailerons of similar sizes
A flight investigation was conducted to determine the lateral-control characteristics of retractable...
Results and discussion are presented of a low-speed lateral-control investigation of three untapered...
This paper presents the results of an investigation to determine the control-effectiveness character...
This report presents the results of wind-tunnel tests made on three model wings having different siz...
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 is the fourth of a series on systematic tests conducted which compares lateral control d...
Since the recent more or less extensive adoption of high-lift flaps on airplane wings, the problem o...
Three model wings, two with typical slotted ailerons and one with typical frise ailerons, have been ...
Combinations of an NACA 23012 tapered wing and a circular fuselage having a wedge-shaped rear were t...
A flight investigation was conducted to determine the lateral-control characteristics of retractable...
Results and discussion are presented of a low-speed lateral-control investigation of three untapered...
This paper presents the results of an investigation to determine the control-effectiveness character...
This report presents the results of wind-tunnel tests made on three model wings having different siz...
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 is the fourth of a series on systematic tests conducted which compares lateral control d...
Since the recent more or less extensive adoption of high-lift flaps on airplane wings, the problem o...
Three model wings, two with typical slotted ailerons and one with typical frise ailerons, have been ...
Combinations of an NACA 23012 tapered wing and a circular fuselage having a wedge-shaped rear were t...
A flight investigation was conducted to determine the lateral-control characteristics of retractable...
Results and discussion are presented of a low-speed lateral-control investigation of three untapered...
This paper presents the results of an investigation to determine the control-effectiveness character...