Add to ORKGThis is the thirteenth report on a series of systematic tests comparing lateral control devices with particular reference to their effectiveness at high angles of attack. The present wind tunnel tests were made to determine the most feasible locations for lateral control surfaces mounted externally to a rectangular Clark y wing
This report is the third of a series giving the results obtained in the 20-foot wind tunnel on the i...
This report is the second of a series giving the results obtained in the 20-foot wind tunnel of the ...
Tests were made with ordinary flap-type ailerons on two wings with different amounts of taper, one m...
A summary has been made of the available information on lateral control. A discussion is given of th...
The results of a wind-tunnel investigation of the NACA 23012, the NACA 23021, and the Clark Y airfoi...
Results are given of a series of systemic tests comparing lateral control devices with particular re...
This report presents the results of flight tests made to determine the lateral control characteristi...
This report presents the results of flight tests made on five different lateral control devices that...
Report presents an investigation carried out in the NACA 7- by 10-foot wind tunnel of an NACA 23012 ...
This report presents the results of wind tunnel tests conducted to determine the aerodynamic charact...
This report is the fourth of a series on systematic tests conducted which compares lateral control d...
Three model wings, two with typical slotted ailerons and one with typical frise ailerons, have been ...
The theory of wind tunnel boundary influence on the downwash from a wing has been extended to provid...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
This report combines the wind tunnel results of tests on four control surface models made in the two...
This report is the third of a series giving the results obtained in the 20-foot wind tunnel on the i...
This report is the second of a series giving the results obtained in the 20-foot wind tunnel of the ...
Tests were made with ordinary flap-type ailerons on two wings with different amounts of taper, one m...
A summary has been made of the available information on lateral control. A discussion is given of th...
The results of a wind-tunnel investigation of the NACA 23012, the NACA 23021, and the Clark Y airfoi...
Results are given of a series of systemic tests comparing lateral control devices with particular re...
This report presents the results of flight tests made to determine the lateral control characteristi...
This report presents the results of flight tests made on five different lateral control devices that...
Report presents an investigation carried out in the NACA 7- by 10-foot wind tunnel of an NACA 23012 ...
This report presents the results of wind tunnel tests conducted to determine the aerodynamic charact...
This report is the fourth of a series on systematic tests conducted which compares lateral control d...
Three model wings, two with typical slotted ailerons and one with typical frise ailerons, have been ...
The theory of wind tunnel boundary influence on the downwash from a wing has been extended to provid...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
This report combines the wind tunnel results of tests on four control surface models made in the two...
This report is the third of a series giving the results obtained in the 20-foot wind tunnel on the i...
This report is the second of a series giving the results obtained in the 20-foot wind tunnel of the ...
Tests were made with ordinary flap-type ailerons on two wings with different amounts of taper, one m...