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Static Thrust Vectoring Performance Of Nonaxisymmetric Convergent Divergent Nozzles With Post Exit Yaw Vanes
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Book Synopsis Static Thrust-vectoring Performance of Nonaxisymmetric Convergent-divergent Nozzles with Post-exit Yaw Vanes by : Robert J. Foley
Download or read book Static Thrust-vectoring Performance of Nonaxisymmetric Convergent-divergent Nozzles with Post-exit Yaw Vanes written by Robert J. Foley and published by . This book was released on 1991 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 :9781722772338 Total Pages :76 pages Book Rating :4.7/5 (723 download)
Book Synopsis Static Performance of Nonaxisymmetric Nozzles with Yaw Thrust-Vectoring Vanes by : National Aeronautics and Space Administration (NASA)
Download or read book Static Performance of Nonaxisymmetric Nozzles with Yaw Thrust-Vectoring Vanes written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-10 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: A static test was conducted in the static test facility of the Langley 16 ft Transonic Tunnel to evaluate the effects of post exit vane vectoring on nonaxisymmetric nozzles. Three baseline nozzles were tested: an unvectored two dimensional convergent nozzle, an unvectored two dimensional convergent-divergent nozzle, and a pitch vectored two dimensional convergent-divergent nozzle. Each nozzle geometry was tested with 3 exit aspect ratios (exit width divided by exit height) of 1.5, 2.5 and 4.0. Two post exit yaw vanes were externally mounted on the nozzle sidewalls at the nozzle exit to generate yaw thrust vectoring. Vane deflection angle (0, -20 and -30 deg), vane planform and vane curvature were varied during the test. Results indicate that the post exit vane concept produced resultant yaw vector angles which were always smaller than the geometric yaw vector angle. Losses in resultant thrust ratio increased with the magnitude of resultant yaw vector angle. The widest post exit vane produced the largest degree of flow turning, but vane curvature had little effect on thrust vectoring. Pitch vectoring was independent of yaw vectoring, indicating that multiaxis thrust vectoring is feasible for the nozzle concepts tested. Mason, Mary L. and Berrier, Bobby L. Langley Research Center...
Book Synopsis Static Performance of an Axisymmetric Nozzle with Post-exit Vanes for Multiaxis Thrust Vectoring by : Bobby L. Berrier
Download or read book Static Performance of an Axisymmetric Nozzle with Post-exit Vanes for Multiaxis Thrust Vectoring written by Bobby L. Berrier and published by . This book was released on 1988 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Performance of Nonaxisymmetric Nozzles with Yaw Thrust-vectoring Vanes by : Mary L. Mason
Download or read book Static Performance of Nonaxisymmetric Nozzles with Yaw Thrust-vectoring Vanes written by Mary L. Mason and published by . This book was released on 1988 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722772215 Total Pages :52 pages Book Rating :4.7/5 (722 download)
Book Synopsis Static Performance of an Axisymmetric Nozzle with Post-Exit Vanes for Multiaxis Thrust Vectoring by : National Aeronautics and Space Administration (NASA)
Download or read book Static Performance of an Axisymmetric Nozzle with Post-Exit Vanes for Multiaxis Thrust Vectoring 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 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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...
Download or read book NASA Technical Paper written by and published by . This book was released on 1995 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NASA Technical Paper by : United States. National Aeronautics and Space Administration
Download or read book NASA Technical Paper written by United States. National Aeronautics and Space Administration and published by . This book was released on 1991 with total page 418 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Performance of Nonaxisymmetric Nozzles with Yaw Thrust-vectoring Vanes by : Mary L. Mason
Download or read book Static Performance of Nonaxisymmetric Nozzles with Yaw Thrust-vectoring Vanes written by Mary L. Mason and published by . This book was released on 1988 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Investigation of Several Yaw Vectoring Concepts on Nonaxisymmetric Nozzles by : Mary L. Mason
Download or read book Static Investigation of Several Yaw Vectoring Concepts on Nonaxisymmetric Nozzles written by Mary L. Mason and published by . This book was released on 1985 with total page 224 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Internal Performance of an Axisymmetric Nozzle with Multiaxis Thrust-vectoring Capability by : George T. Carson
Download or read book Static Internal Performance of an Axisymmetric Nozzle with Multiaxis Thrust-vectoring Capability written by George T. Carson and published by . This book was released on 1991 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1991 with total page 1102 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NASA Scientific and Technical Publications by :
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:
Book Synopsis NASA Scientific and Technical Publications: A Catalog of Special Publications, Reference Publications, Conference Publications, and Technical Papers, 1991-1992 by :
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:
Book Synopsis Effects of Internal Yaw-vectoring Devices on the Static Performance of a Pitch-vectoring Nonaxisymmetric Convergent-divergent Nozzle by : Scott C. Asbury
Download or read book Effects of Internal Yaw-vectoring Devices on the Static Performance of a Pitch-vectoring Nonaxisymmetric Convergent-divergent Nozzle written by Scott C. Asbury and published by . This book was released on 1993 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Vectored Propulsion, Supermaneuverability and Robot Aircraft by : Benjamin Gal-Or
Download or read book Vectored Propulsion, Supermaneuverability and Robot Aircraft written by Benjamin Gal-Or and published by Springer Science & Business Media. This book was released on 2013-11-09 with total page 277 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book is designed to fill a professional vacuum in the new field of advance, high-angle, vectored stealth aircraft. The subject matter presented in the volume has never before been investigated and presented as a unified field of study because it covers entirely new fields and because specialized fragments of this unified field are scattered throughout literature in specific problems. The book is of interest to aeronautical and mechanical engineers, electrical and control engineers, aerospace industry, USAF, US Navy, NASA, pilots and instructors.
Book Synopsis Static Performance of a Cruciform Nozzle with Multiaxis Thrust-vectoring and Reverse-thrust Capabilities by : David J. Wing
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:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1988 with total page 1142 pages. Available in PDF, EPUB and Kindle. Book excerpt: