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Author: National Aeronautics and Space Adm Nasa Publisher: Independently Published ISBN: 9781730709913 Category : Science Languages : en Pages : 54
Book Description
An investigation was conducted in the static test facility of the Langley 16-Foot Transonic Tunnel to determine the flow-turning capability and the nozzle internal performance of an axisymmetric convergent-divergent nozzle with post-exit vanes installed for multiaxis thrust vectoring. The effects of vane curvature, vane location relative to the nozzle exit, number of vanes, and vane deflection angle were determined. A comparison of the post-exit-vane thrust-vectoring concept with other thrust-vectoring concepts is provided. All tests were conducted with no external flow, and nozzle pressure ratio was varied from 1.6 to 6.0. Berrier, Bobby L. and Mason, Mary L. Langley Research Center...
Author: National Aeronautics and Space Adm Nasa Publisher: Independently Published ISBN: 9781730709913 Category : Science Languages : en Pages : 54
Book Description
An investigation was conducted in the static test facility of the Langley 16-Foot Transonic Tunnel to determine the flow-turning capability and the nozzle internal performance of an axisymmetric convergent-divergent nozzle with post-exit vanes installed for multiaxis thrust vectoring. The effects of vane curvature, vane location relative to the nozzle exit, number of vanes, and vane deflection angle were determined. A comparison of the post-exit-vane thrust-vectoring concept with other thrust-vectoring concepts is provided. All tests were conducted with no external flow, and nozzle pressure ratio was varied from 1.6 to 6.0. Berrier, Bobby L. and Mason, Mary L. Langley Research Center...
Author: National Aeronautics and Space Adm Nasa
Author: Bobby L. Berrier
Author: National Aeronautics and Space Adm Nasa
Author: David J. Wing
Author: 
Author: George T. Carson (Jr.)
Author: George T. Carson
Author: Robert J. Foley
Author: Mary L. Mason
Author: Mary L. Mason
Author: