Static Performance Of A Cruciform Nozzle With Multiaxis Thrust Vectoring And Reverse Thrust Capabilities

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Static Performance Of A Cruciform Nozzle With Multiaxis Thrust Vectoring And Reverse Thrust Capabilities

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Author : David J. Wing
language : en
Publisher:
Release Date : 1992

Static Performance Of A Cruciform Nozzle With Multiaxis Thrust Vectoring And Reverse Thrust Capabilities written by David J. Wing and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Airplanes categories.

Static Performance Investigation Of A Skewed Throat Multiaxis Thrust Vectoring Nozzle Concept

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Author : David J. Wing
language : en
Publisher:
Release Date : 1994

Static Performance Investigation Of A Skewed Throat Multiaxis Thrust Vectoring Nozzle Concept written by David J. Wing and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with categories.

Static Performance Of A Cruciform Nozzle With Multiaxis Thrust Vectoring And Reverse Thrust Capabilities

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Author : David J. Wing
language : en
Publisher:
Release Date : 1992

Static Performance Of A Cruciform Nozzle With Multiaxis Thrust Vectoring And Reverse Thrust Capabilities written by David J. Wing and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with categories.

Nasa Technical Paper

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Author :
language : en
Publisher:
Release Date : 1992

Nasa Technical Paper written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Science categories.

Nasa Technical Paper

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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1992

Nasa Technical Paper written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Aeronautics categories.

Nasa Scientific And Technical Publications

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Author :
language : en
Publisher:
Release Date : 1993

Nasa Scientific And Technical Publications written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993 with Aeronautics categories.

Static Performance Of A Cruciform Nozzle With Multiaxis Thrust Vectoring And Reverse Thrust Capabilities

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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-07-16

Static Performance Of A Cruciform Nozzle With Multiaxis Thrust Vectoring And Reverse Thrust Capabilities written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-07-16 with categories.

A multiaxis thrust vectoring nozzle designed to have equal flow turning capability in pitch and yaw was conceived and experimentally tested for internal, static performance. The cruciform-shaped convergent-divergent nozzle turned the flow for thrust vectoring by deflecting the divergent surfaces of the nozzle, called flaps. Methods for eliminating physical interference between pitch and yaw flaps at the larger multiaxis deflection angles was studied. These methods included restricting the pitch flaps from the path of the yaw flaps and shifting the flow path at the throat off the nozzle centerline to permit larger pitch-flap deflections without interfering with the operation of the yaw flaps. Two flap widths were tested at both dry and afterburning settings. Vertical and reverse thrust configurations at dry power were also tested. Comparison with two dimensional convergent-divergent nozzles showed lower but still competitive thrust performance and thrust vectoring capability. Wing, David J. and Asbury, Scott C. Langley Research Center...

Isolated Performance At Mach Numbers From 0 60 To 2 86 Of Several Expendable Nozzle Concepts For Supersonic Applications

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Author : Richard J. Re
language : en
Publisher:
Release Date : 2001

Isolated Performance At Mach Numbers From 0 60 To 2 86 Of Several Expendable Nozzle Concepts For Supersonic Applications written by Richard J. Re and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2001 with Mach number categories.

Investigations have been conducted in the Langley 16-Foot Transonic Tunnel (at Mach numbers from 0.60 to 1.25) and in the Langley Unitary Plan Winf Tunnel (at Mach numbers from 2.16 to 2.86) at an angle of attack of O° to determine the isolated performane of several expendable nozzle concepts for supersonic noaugmented turbojet applications. The effects of centerbody base shape, shroud length, shroud ventilation, cruciform shroud expansion ration, and cruciform shroud flap vectoring were investigated. The nozzle pressure ration range, which was a function of Mach number, was between 1.9 and 11.8 in the 16-Foot Transonic Tunnel and between 7.9 and 54.9 in the Unitary Plan WInd Tunnel. Discharge coefficient, thrust-minus-drag, and the forces and moments generated by vectoring the divergent shroud flaps (for Mach numbers of 0.60 to 1.25 only) of a cruciform nozzle configuration were measured.

Scientific And Technical Aerospace Reports

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Author :
language : en
Publisher:
Release Date : 1992

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Aeronautics categories.

Monthly Catalog Of United States Government Publications

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Author : United States. Superintendent of Documents
language : en
Publisher:
Release Date : 1993

Monthly Catalog Of United States Government Publications written by United States. Superintendent of Documents and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993 with Government publications categories.