Add to ORKGThis report presents the results of wind tunnel tests to determine the effectiveness of various methods of reducing the high control forces of unbalanced upper-surface ailerons and of unbalanced split flaps
A flight investigation was conducted to determine the lateral-control characteristics of retractable...
This report contains the results obtained at the Langley Memorial Aeronautical Laboratory on an N. A...
Discussed here are a series of systematic tests being conducted to compare different lateral control...
This report covers the twelfth of a series of tests conducted to compare different lateral control d...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel to determi...
Three model wings, two with typical slotted ailerons and one with typical frise ailerons, have been ...
Tests were made on a model wing with three different sized split trailing-edged flaps, in the NACA 7...
A large-chord NACA 23012 airfoil was tested. The airfoil extended completely across the test section...
This report covers the sixth of a series of investigations in which various lateral control devices ...
This report is the fourth of a series on systematic tests conducted which compares lateral control d...
Flat-plate flaps with no wing cutouts and flaps having Clark Y sections with corresponding cutouts m...
Tests were made with ordinary flap-type ailerons on two wings with different amounts of taper, one m...
Aerodynamic force tests were made in the N.A.C.A. 7 by 10 foot wind tunnel on a model Clark Y wing w...
Report presents the results of wind tunnel tests of the Clark Y, the NACA 23012 and the NACA 23021 a...
Report presents the results of an extensive investigation made in the NACA 7 by 10-foot wind tunnel ...
A flight investigation was conducted to determine the lateral-control characteristics of retractable...
This report contains the results obtained at the Langley Memorial Aeronautical Laboratory on an N. A...
Discussed here are a series of systematic tests being conducted to compare different lateral control...
This report covers the twelfth of a series of tests conducted to compare different lateral control d...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel to determi...
Three model wings, two with typical slotted ailerons and one with typical frise ailerons, have been ...
Tests were made on a model wing with three different sized split trailing-edged flaps, in the NACA 7...
A large-chord NACA 23012 airfoil was tested. The airfoil extended completely across the test section...
This report covers the sixth of a series of investigations in which various lateral control devices ...
This report is the fourth of a series on systematic tests conducted which compares lateral control d...
Flat-plate flaps with no wing cutouts and flaps having Clark Y sections with corresponding cutouts m...
Tests were made with ordinary flap-type ailerons on two wings with different amounts of taper, one m...
Aerodynamic force tests were made in the N.A.C.A. 7 by 10 foot wind tunnel on a model Clark Y wing w...
Report presents the results of wind tunnel tests of the Clark Y, the NACA 23012 and the NACA 23021 a...
Report presents the results of an extensive investigation made in the NACA 7 by 10-foot wind tunnel ...
A flight investigation was conducted to determine the lateral-control characteristics of retractable...
This report contains the results obtained at the Langley Memorial Aeronautical Laboratory on an N. A...
Discussed here are a series of systematic tests being conducted to compare different lateral control...