Add to ORKGThis investigation was undertaken to determine the relative effects of those factors which may interfere with the rudder control of an airplane, with especial reference to the process of landing. It shows that ground interference is negligible, but that the effects of a large rounded body and of the slip stream may combine to interfere seriously with rudder control at low flying speeds and when taxiing
The conditions which must be met at the slipstream boundary are developed, after which it is shown w...
This report presents the results of full-scale tests made on a 10-foot 5-inch propeller on a geared ...
The object of the investigation described in this report was to compare the damping coefficients of ...
The horizontal tail surfaces of a new airplane usually are proportional so that the curve of moment ...
The screw propeller on airplanes is usually placed near other objects, and hence its performance may...
This investigation was undertaken to determine the relative effects of those factors which may inter...
The results of wind tunnel tests for the determination of the effect of a jet on the lift and downwa...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
Report presents the results of an investigation of the effects of ground interference on the aerodyn...
This report gives the results of tests on a rectangular wing model with a 20% full spun split flap, ...
Results are presented of a flight investigation conducted on a fighter-type airplane to determine th...
On various low-wing monoplanes the horizontal tail surfaces flutter in flight at large angles of att...
To quantify the installed performance of high speed (M = 0.8) turboprop propulsion systems, an exper...
An investigation was conducted to determine the floating characteristics of full-length plain and ho...
This investigation was undertaken for the purpose of developing instruments that would record the fo...
The conditions which must be met at the slipstream boundary are developed, after which it is shown w...
This report presents the results of full-scale tests made on a 10-foot 5-inch propeller on a geared ...
The object of the investigation described in this report was to compare the damping coefficients of ...
The horizontal tail surfaces of a new airplane usually are proportional so that the curve of moment ...
The screw propeller on airplanes is usually placed near other objects, and hence its performance may...
This investigation was undertaken to determine the relative effects of those factors which may inter...
The results of wind tunnel tests for the determination of the effect of a jet on the lift and downwa...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
Report presents the results of an investigation of the effects of ground interference on the aerodyn...
This report gives the results of tests on a rectangular wing model with a 20% full spun split flap, ...
Results are presented of a flight investigation conducted on a fighter-type airplane to determine th...
On various low-wing monoplanes the horizontal tail surfaces flutter in flight at large angles of att...
To quantify the installed performance of high speed (M = 0.8) turboprop propulsion systems, an exper...
An investigation was conducted to determine the floating characteristics of full-length plain and ho...
This investigation was undertaken for the purpose of developing instruments that would record the fo...
The conditions which must be met at the slipstream boundary are developed, after which it is shown w...
This report presents the results of full-scale tests made on a 10-foot 5-inch propeller on a geared ...
The object of the investigation described in this report was to compare the damping coefficients of ...