Motion Induced Aerodynamics of a Pitching Delta Wing
| Author | : Jon Vaughan |
| Publisher | : |
| Total Pages | : |
| Release | : 1997 |
| Genre | : |
| ISBN | : |
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Motion Induced Aerodynamics Of A Pitching Delta Wing
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The Unsteady Aerodynamics of a Delta Wing Undergoing Large Amplitude Pitching Motions
| Author | : Scott Andrew Thompson |
| Publisher | : |
| Total Pages | : 452 |
| Release | : 1992 |
| Genre | : |
| ISBN | : |
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Unsteady Aerodynamics of Delta Wings Performing Maneuvers to High Angle of Attack
| Author | : Mohammad-Ameen M. Jarrah |
| Publisher | : |
| Total Pages | : 352 |
| Release | : 1988 |
| Genre | : Aerodynamics |
| ISBN | : |
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Influence of Airfoil Geometry on Delta Wing Leading-edge Vortices and Vortex-induced Aerodynamics at Supersonic Speeds
| Author | : Richard M. Wood |
| Publisher | : |
| Total Pages | : 88 |
| Release | : 1992 |
| Genre | : Aerodynamics, Supersonic |
| ISBN | : |
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Thrust-induced Effects on a Pitching-up Delta Wing Flow Field
| Author | : Leon L. Van Dommelen |
| Publisher | : |
| Total Pages | : 30 |
| Release | : 1995 |
| Genre | : Airplanes |
| ISBN | : |
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Neural network procedures were explored with the objectives to control a delta wing in the non-linear domain. Results show that neural networks are well suited to represent non-linear computed lift and pressure forces on delta wings. A model problem, the flare maneuver, suggests that neural network controllers can perform well for non-linear systems provided that suitable input and training data are provided to it.
A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0
| Author | : Robert S. Osborne |
| Publisher | : |
| Total Pages | : 20 |
| Release | : 1960 |
| Genre | : Aerodynamics |
| ISBN | : |
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Experimental Determination of Damping in Pitch of Swept and Delta Wings at Supersonic Mach Numbers
| Author | : John A. Moore |
| Publisher | : |
| Total Pages | : 28 |
| Release | : 1957 |
| Genre | : Aerodynamics, Supersonic |
| ISBN | : |
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The damping-in-pitch derivative was determined experimentally at Mach numbers of 2.96 and 3.92 for two delta wings having aspect ratios of 2 and 3 and for one sweptback tapered wing having an aspect ratio of 3 by using a free-oscillation technique. The tests were made at Reynolds numbers based on mean aerodynamic chord from 4,000,000 to 12,000,000 for an angle-of-attack range of zero to 10 degrees. The reduced-frequency parameter ranged from 0.006 to 0.022.
The Unsteady Aerodynamics of a Delta Wing Undergoing Large Amplitude Pitching Motions
| Author | : Scott Andrew Thompson |
| Publisher | : |
| Total Pages | : 0 |
| Release | : 1992 |
| Genre | : |
| ISBN | : |
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Prediction of Unsteady Aerodynamics and Control of Delta Wings with Tangential Leading Edge Blowing
| Author | : Stanford University. Department of Aeronautics and Astronautics |
| Publisher | : |
| Total Pages | : 396 |
| Release | : 1989 |
| Genre | : |
| ISBN | : |
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The Aerodynamic Characteristics of Several Thick Delta Wings at Mach Numbers to 6 and Angles of Attack 50°
| Author | : John B. McDevitt |
| Publisher | : |
| Total Pages | : 114 |
| Release | : 1960 |
| Genre | : Aerodynamics |
| ISBN | : |
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