Add to ORKGForce tests on a systematic series of wing systems over a range of angle of attack from minus forty-five degrees to plus ninety degrees are covered in this report. The investigation was made on monoplane and biplane wing models to determine the effects of variations of tip shape, aspect ratio, flap setting, stagger, gap, decalage, sweepback, and airfoil profile
This report presents the results of an investigation conducted in the Langley 300 mph 7- by 10-foot ...
At the request of the Army Air Corps, an investigation of the pressure distribution over PW-9 wing m...
In this report tests are described in which the distribution of pressures over models of the wings o...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
This report is on the changes in forces on each wing of a biplane cellule when either the stagger or...
This preliminary report furnishes information on the changes in the forces on each wing of a biplane...
This report contains the results of a series of tests with three wing models. By changing the sectio...
This preliminary report furnishes information on the changes in the forces on each wing of a biplane...
The pressure distribution tests described in this report, covering angles of attack up to 90 degrees...
Wind tunnel tests to determine effect of angle of attack on maximum lift at stall for half-wing mode...
Force tests on a systematic series of wing systems over a range of angle of attack from minus forty-...
The model was a full-scale mockup of a light single-engine high-wing monoplane. Tests were made over...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
Wind tunnel tests have been conducted on a research airplane model with an NASA supercritical wing t...
This report presents the results of an investigation conducted in the Langley 300 mph 7- by 10-foot ...
At the request of the Army Air Corps, an investigation of the pressure distribution over PW-9 wing m...
In this report tests are described in which the distribution of pressures over models of the wings o...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
This report is on the changes in forces on each wing of a biplane cellule when either the stagger or...
This preliminary report furnishes information on the changes in the forces on each wing of a biplane...
This report contains the results of a series of tests with three wing models. By changing the sectio...
This preliminary report furnishes information on the changes in the forces on each wing of a biplane...
The pressure distribution tests described in this report, covering angles of attack up to 90 degrees...
Wind tunnel tests to determine effect of angle of attack on maximum lift at stall for half-wing mode...
Force tests on a systematic series of wing systems over a range of angle of attack from minus forty-...
The model was a full-scale mockup of a light single-engine high-wing monoplane. Tests were made over...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
Wind tunnel tests have been conducted on a research airplane model with an NASA supercritical wing t...
This report presents the results of an investigation conducted in the Langley 300 mph 7- by 10-foot ...
At the request of the Army Air Corps, an investigation of the pressure distribution over PW-9 wing m...
In this report tests are described in which the distribution of pressures over models of the wings o...