INVESTIGATION OF THRUST VECTORING METHODS IN EJECTOR AND TURNING NOZZLES |
4 | |
2011 |
scientific article | 533.694.6 | ||
692-693 |
The report presents results of experimental and theoretical investigations of nozzles with thrust vectoring conducted in Central Institute of Aviation Motors. The nozzles includes nozzles with turning supersonic, flat and 3D nozzles with asymmetric ejection of ambient flow, nozzles with injections and interceptors, and nozzles with critical surface shifting. |
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