Add to ORKGThis preliminary report furnishes information on the changes in the forces on each wing of a biplane cellule for various combinations of stagger and gap, stagger and sweepback, stagger and decalage, and gap and decalage. The data were obtained from pressure distribution tests made in the atmospheric wind tunnel of the Langley Memorial Aeronautical Laboratory. Since each test was carried up to 90deg angle of attack, the results may be used in the study of stalled flight and of spinning as well as in the structural design of biplane wings
In this report ~est~are described in which. the distribution OJpressures omr modek of tlie un”ngs of...
This note presents the results obtained in pressure distribution tests on the right upper panel of a...
This paper is the first of a series of notes, each of which presents the complete results of pressur...
This preliminary report furnishes information on the changes in the forces on each wing of a biplane...
This report is on the changes in forces on each wing of a biplane cellule when either the stagger or...
Force tests on a systematic series of wing systems over a range of angle of attack from minus forty-...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
This preliminary report furnishes information on the changes in the forces on each wing of a biplane...
It is known that in a biplane the load is not distributed equally between the wings. The presence of...
In this report tests are described in which the distribution of pressures over models of the wings o...
This investigation was carried out by request of the United States Air Service at the Massachusetts ...
This note presents the results of flight pressure-distribution tests on the right upper wing panel o...
At the request of the Army Air Corps, an investigation of the pressure distribution over PW-9 wing m...
This note presents the results of flight pressure-distribution tests on the right upper wing panel o...
Measurements of wing and fuselage pressure distributions were made at low and high subsonic Much num...
In this report ~est~are described in which. the distribution OJpressures omr modek of tlie un”ngs of...
This note presents the results obtained in pressure distribution tests on the right upper panel of a...
This paper is the first of a series of notes, each of which presents the complete results of pressur...
This preliminary report furnishes information on the changes in the forces on each wing of a biplane...
This report is on the changes in forces on each wing of a biplane cellule when either the stagger or...
Force tests on a systematic series of wing systems over a range of angle of attack from minus forty-...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
This preliminary report furnishes information on the changes in the forces on each wing of a biplane...
It is known that in a biplane the load is not distributed equally between the wings. The presence of...
In this report tests are described in which the distribution of pressures over models of the wings o...
This investigation was carried out by request of the United States Air Service at the Massachusetts ...
This note presents the results of flight pressure-distribution tests on the right upper wing panel o...
At the request of the Army Air Corps, an investigation of the pressure distribution over PW-9 wing m...
This note presents the results of flight pressure-distribution tests on the right upper wing panel o...
Measurements of wing and fuselage pressure distributions were made at low and high subsonic Much num...
In this report ~est~are described in which. the distribution OJpressures omr modek of tlie un”ngs of...
This note presents the results obtained in pressure distribution tests on the right upper panel of a...
This paper is the first of a series of notes, each of which presents the complete results of pressur...