Add to ORKGAn investigation of the rolling effectiveness at transonic and supersonic speeds of partial-span ailerons on a 42.7 degree sweptback wing having symmetrical circular-arc airfoil sections of 10-percent thickness ratio normal to the wing quarter-chord line has been made by means of rocket-propelled test vehicles. The results are compared with results of a supersonic wind-tunnel test at Mach number 1.9
An investigation of the flutter characteristics of a series of thin cantilever wings having taper ra...
Results are presented of brief flight tests of the aileron characteristics of the XP-60 airplane wit...
An analysis is presented of the effect of torsional flexibility on the rolling characteristics at su...
An investigation of the rolling effectiveness at transonic and supersonic speeds of partial-span ail...
The effect of spsnwise aileron location on the rolling effective-ness of 0.2-chord plain faired aile...
A three-dimensional investigation of straight-sided-profile plain ailerons on a wing with 30 degrees...
An investigation has been conducted in the Langley 4- by 4-foot supersonic tunnel at Mach numbers 1....
Damping-in-roll coefficients for a series of triangular plan-form wings and two rectangular plan-for...
A method is presented for calculating the steady-state rolling effectiveness of ~lexible sweptback w...
A summary and analysis have been made of the results of various investigations to determine the aero...
An analysis of the principal results of recent control-surface research pertinent to transonic fligh...
In the course of a flight test of a supersonic research pilotless aircraft (the NACA RM-1), large-am...
The aerodynamic roll damping and the yawing moment due to roll rate characteristics were investigate...
' s u " m Y A n investigation at subscwic and transonic speeds has been performsd in the L...
Aileron effectiveness for a subsonc energy efficient transport (EET) model with a high aspect ratio ...
An investigation of the flutter characteristics of a series of thin cantilever wings having taper ra...
Results are presented of brief flight tests of the aileron characteristics of the XP-60 airplane wit...
An analysis is presented of the effect of torsional flexibility on the rolling characteristics at su...
An investigation of the rolling effectiveness at transonic and supersonic speeds of partial-span ail...
The effect of spsnwise aileron location on the rolling effective-ness of 0.2-chord plain faired aile...
A three-dimensional investigation of straight-sided-profile plain ailerons on a wing with 30 degrees...
An investigation has been conducted in the Langley 4- by 4-foot supersonic tunnel at Mach numbers 1....
Damping-in-roll coefficients for a series of triangular plan-form wings and two rectangular plan-for...
A method is presented for calculating the steady-state rolling effectiveness of ~lexible sweptback w...
A summary and analysis have been made of the results of various investigations to determine the aero...
An analysis of the principal results of recent control-surface research pertinent to transonic fligh...
In the course of a flight test of a supersonic research pilotless aircraft (the NACA RM-1), large-am...
The aerodynamic roll damping and the yawing moment due to roll rate characteristics were investigate...
' s u " m Y A n investigation at subscwic and transonic speeds has been performsd in the L...
Aileron effectiveness for a subsonc energy efficient transport (EET) model with a high aspect ratio ...
An investigation of the flutter characteristics of a series of thin cantilever wings having taper ra...
Results are presented of brief flight tests of the aileron characteristics of the XP-60 airplane wit...
An analysis is presented of the effect of torsional flexibility on the rolling characteristics at su...