Investigation Over Moving Ground Plane of a Transport Airplane Model Using Blowing Over Flaps for Boundary-layer Control
Author | : Raymond D. Vogler |
Publisher | : |
Total Pages | : 90 |
Release | : 1967 |
Genre | : Stability of airplanes, Longitudinal |
ISBN | : |
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Author | : Raymond D. Vogler |
Publisher | : |
Total Pages | : 90 |
Release | : 1967 |
Genre | : Stability of airplanes, Longitudinal |
ISBN | : |
Author | : Raymond D. Vogler |
Publisher | : |
Total Pages | : 52 |
Release | : 1970 |
Genre | : Airplanes |
ISBN | : |
Ground effects investigation of STOL air-sea transport model with blowing over canard and wing flaps.
Author | : United States. Superintendent of Documents |
Publisher | : |
Total Pages | : 1214 |
Release | : 1967-07 |
Genre | : Government publications |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 428 |
Release | : 1968 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 436 |
Release | : 1968 |
Genre | : Aeronautics |
ISBN | : |
Author | : C. Thomas Snyder |
Publisher | : |
Total Pages | : 60 |
Release | : 1970 |
Genre | : Airplanes |
ISBN | : |
The influence of ground effect on the landing flare characteristics of a supersonic transport airplane (SST) was investigated in a fixed cockpit simulator. Simulations of an ogee-modified delta-wing F5D-1 airplane and a subsonic jet transport were used for evaluating the simulator and as a reference configurations during landing comparisons. Dynamic responses of the SST to seven different ground-effect models during controls-fixed and constant-attitude descents are also presented, followed by piloted subjective assessments. A summary of ground effects on delta-like wings is included in the appendixes.