Attention is given to the prediction of lift-system-induced aerodynamic effects in lift-jet VTOL aircraft, considering both analytical fluid-dynamics models and an empirical database. The methodology takes into account the effects of aircraft geometry and orientation as well as height above ground, lift-jet vector and splay directions, jet exit-flow conditions, and nozzle exit geometry.
Multiple jet impingement flowfields
1986-01-01
Miscellaneous
No indication
English
Computations and measurements of two-dimensional turbulent jet impingement flowfields
Tema Archive | 1977
|AIAA | 1983
|Supersonic reacting internal flowfields
NTRS | 1991
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