Flight tests were carried out at the Langley Field laboratory of the NACA, on several airplanes for the purpose of determining their relative performance with the same engine and the same propeller. The method used consisted in flying each airplane on a level course and measuring the airspeed for the whole range of engine revolutions. In general the results show that a small change in the wing section or the wing area has but a slight effect upon the performance, but changes in those parts which cause the structural resistance have a very important effect
This report is a listing of the different studies conducted by the Institute in May thru August of 1...
Calculations of the magnitude of the correction factors and the range of their variations for wind t...
An investigation was conducted in the NACA full-scale wind tunnel to determine the drag and the prop...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
Aerodynamic tests were made with four geometrically similar metal propellers of different diameters,...
This investigation was made for the purpose of determining the characteristics of five full-scale pr...
In order to determine the effect of the surface conditions of a wing on the aerodynamic characterist...
Flight tests were carried out at the Langley Field laboratory of the NACA, on several airplanes for ...
Data are presented to show the extent to which the maximum lift coefficient and consequently the min...
In order to determine the efficiency of a propeller as accurately as possible, its revolution speed,...
An investigation was conducted to determine the effect of the wings on propulsive efficiency. The wi...
Tests were made to determine the effect of fillets between wings and fuselage on the drag and propul...
An adjustable blade metal propeller was tested at five different angle settings, forming a series va...
This report, prepared at the request of the NACA, describes tests of three metal model propellers, i...
This report presents the results of flight tests with three different airplanes using several types ...
This report is a listing of the different studies conducted by the Institute in May thru August of 1...
Calculations of the magnitude of the correction factors and the range of their variations for wind t...
An investigation was conducted in the NACA full-scale wind tunnel to determine the drag and the prop...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
Aerodynamic tests were made with four geometrically similar metal propellers of different diameters,...
This investigation was made for the purpose of determining the characteristics of five full-scale pr...
In order to determine the effect of the surface conditions of a wing on the aerodynamic characterist...
Flight tests were carried out at the Langley Field laboratory of the NACA, on several airplanes for ...
Data are presented to show the extent to which the maximum lift coefficient and consequently the min...
In order to determine the efficiency of a propeller as accurately as possible, its revolution speed,...
An investigation was conducted to determine the effect of the wings on propulsive efficiency. The wi...
Tests were made to determine the effect of fillets between wings and fuselage on the drag and propul...
An adjustable blade metal propeller was tested at five different angle settings, forming a series va...
This report, prepared at the request of the NACA, describes tests of three metal model propellers, i...
This report presents the results of flight tests with three different airplanes using several types ...
This report is a listing of the different studies conducted by the Institute in May thru August of 1...
Calculations of the magnitude of the correction factors and the range of their variations for wind t...
An investigation was conducted in the NACA full-scale wind tunnel to determine the drag and the prop...