Wind Tunnel Investigation Of The Aerodynamic And Structural Deflection Characteristics Of The Goodyear Inflatoplane
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| Author | : Bennie W. Cocke (Jr.) |
| Publisher | : |
| Total Pages | : 62 |
| Release | : 1958 |
| Genre | : Aerodynamic load |
| ISBN | : |
Summary: An investigation has been conducted in the Langley full-scale tunnel to determine the aerodynamic and structural deflection characteristics of the Goodyear Inflatoplane over a range of test velocities from minimum stall speed up to speeds giving load factors for wing buckling. Tests were conducted over a range of speeds from approximately 41 to 70 mph with wing-guy-cable loads, wing-distortion photographs, and aerodynamic-force data recorded at each speed for a full range of angle of attack.
| Author | : H. C. Mc Lemore |
| Publisher | : |
| Total Pages | : 208 |
| Release | : 1962 |
| Genre | : Airplanes |
| ISBN | : |
Tests were conducted in the Langley full-scale tunnel for a range of speeds from minimum stall speed to speeds at which it was possible to produce a load factor sufficient to cause wing buckling. Static aerodynamic and control data, wing-pressure-distribution data, wing-deflection photographs, and wing-guy-cable loads are presented. Results of the tests show that a maximum load factor of the order of 4.50 can be attained for a normal inflation pressure of 7.0 lb/sq in.
| Author | : |
| Publisher | : |
| Total Pages | : 618 |
| Release | : 1993 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 388 |
| Release | : 1959 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 388 |
| Release | : 1957 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 520 |
| Release | : 1992 |
| Genre | : Astronautics |
| ISBN | : |
| Author | : Bennie W. Cocke (Jr.) |
| Publisher | : |
| Total Pages | : 64 |
| Release | : 19?? |
| Genre | : Aerodynamics |
| ISBN | : |
Summary: An investigation has been conducted in the Langley full-scale tunnel to determine the aerodynamic and structural deflection characteristics of the Goodyear Inflatoplane over a range of test velocities from minimum stall speed up to speeds giving load factors for wing buckling. Tests were conducted over a range of speeds from approximately 41 to 70 mph with wing-guy-cable loads, wing-distortion photographs, and aerodynamic-force data recorded at each speed for a full range of angle of attack.
| Author | : |
| Publisher | : |
| Total Pages | : 1698 |
| Release | : 1959 |
| Genre | : Government publications |
| ISBN | : |
| Author | : Defense Documentation Center (U.S.) |
| Publisher | : |
| Total Pages | : 1116 |
| Release | : 1961-02 |
| Genre | : Technology |
| ISBN | : |
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 716 |
| Release | : 1956 |
| Genre | : Aeronautics |
| ISBN | : |
