Add to ORKGIn the subdivided wing section profile, the diagram of the current is entirely changed and the harmful formation of eddies is avoided through premature deflection. Pressure equalization does not occur between the upper and under sides. This report presents a discussion of the various laws relating to wing design with the conclusion being that lift increases with more acute angles of attack
The causes of error in experiments conducted in wind tunnel tests are given and the value of in-flig...
This preliminary report furnishes information on the changes in the forces on each wing of a biplane...
Aerodynamic considerations led us, not long ago, to investigate a device which seemed to promise a c...
Discussed here are the aerodynamics of a subdivided wing section. The emphasis is upon the increase ...
In the subdivided wing section profile, the diagram of the current is entirely changed and the harmf...
Wind-tunnel tests are described, in which the angle of attack of a wing model was suddenly increased...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
Force tests on a systematic series of wing systems over a range of angle of attack from minus forty-...
Tests were made on a model wing with three different sized split trailing-edged flaps, in the NACA 7...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
Since the war there has been a considerable advance in knowledge on the subject of the airfoil and i...
The historical development of the rules for structural strength of aircraft in the leading countries...
This report gives a simple and exact method of calculating the lift distribution on thin wing sectio...
Determinations of the power-off maximum lift of a Fairchild 22 airplane were made in the NACA full-s...
The causes of error in experiments conducted in wind tunnel tests are given and the value of in-flig...
This preliminary report furnishes information on the changes in the forces on each wing of a biplane...
Aerodynamic considerations led us, not long ago, to investigate a device which seemed to promise a c...
Discussed here are the aerodynamics of a subdivided wing section. The emphasis is upon the increase ...
In the subdivided wing section profile, the diagram of the current is entirely changed and the harmf...
Wind-tunnel tests are described, in which the angle of attack of a wing model was suddenly increased...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
Force tests on a systematic series of wing systems over a range of angle of attack from minus forty-...
Tests were made on a model wing with three different sized split trailing-edged flaps, in the NACA 7...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
Since the war there has been a considerable advance in knowledge on the subject of the airfoil and i...
The historical development of the rules for structural strength of aircraft in the leading countries...
This report gives a simple and exact method of calculating the lift distribution on thin wing sectio...
Determinations of the power-off maximum lift of a Fairchild 22 airplane were made in the NACA full-s...
The causes of error in experiments conducted in wind tunnel tests are given and the value of in-flig...
This preliminary report furnishes information on the changes in the forces on each wing of a biplane...
Aerodynamic considerations led us, not long ago, to investigate a device which seemed to promise a c...