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

Author : David J. Wing
Publisher :
ISBN 13 :
Total Pages : 88 pages
Book Rating : 4.42/5 ( download)

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Download or read book Static Performance of a Cruciform Nozzle with Multiaxis Thrust-vectoring and Reverse-thrust Capabilities written by David J. Wing and published by . This book was released on 1992 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722771683
Total Pages : 82 pages
Book Rating : 4.82/5 ( download)

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Download or read book Static Performance of a Cruciform Nozzle with Multiaxis Thrust-Vectoring and Reverse-Thrust Capabilities written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-16 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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...

Author : David J. Wing
Publisher :
ISBN 13 :
Total Pages : 132 pages
Book Rating : 4.03/5 ( download)

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Download or read book Static Performance Investigation of a Skewed-throat Multiaxis Thrust-vectoring Nozzle Concept written by David J. Wing and published by . This book was released on 1994 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : David J. Wing
Publisher :
ISBN 13 :
Total Pages : 88 pages
Book Rating : 4.15/5 ( download)

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Download or read book Static Performance of a Cruciform Nozzle with Multiaxis Thrust-vectoring and Reverse-thrust Capabilities written by David J. Wing and published by . This book was released on 1992 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author :
Publisher :
ISBN 13 :
Total Pages : 90 pages
Book Rating : 4.13/5 ( download)

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Download or read book NASA Technical Paper written by and published by . This book was released on 1992 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : United States. National Aeronautics and Space Administration
Publisher :
ISBN 13 :
Total Pages : 88 pages
Book Rating : 4.23/5 ( download)

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Download or read book NASA Technical Paper written by United States. National Aeronautics and Space Administration and published by . This book was released on 1992 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author :
Publisher :
ISBN 13 :
Total Pages : 134 pages
Book Rating : 4.56/5 ( download)

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Download or read book NASA Scientific and Technical Publications written by and published by . This book was released on 1993 with total page 134 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author :
Publisher :
ISBN 13 :
Total Pages : 122 pages
Book Rating : 4.68/5 ( download)

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Download or read book NASA Scientific and Technical Publications: A Catalog of Special Publications, Reference Publications, Conference Publications, and Technical Papers, 1991-1992 written by and published by . This book was released on 1993 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Richard J. Re
Publisher :
ISBN 13 :
Total Pages : 202 pages
Book Rating : 4.33/5 ( download)

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Download or read book 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 published by . This book was released on 2001 with total page 202 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Author :
Publisher :
ISBN 13 :
Total Pages : 1572 pages
Book Rating : 4.13/5 ( download)

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Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1992 with total page 1572 pages. Available in PDF, EPUB and Kindle. Book excerpt: