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Performance Of Twin Two Dimensional Wedge Nozzles Including Thrust Vectoring And Reversing Effects At Speeds Up To Mach 220
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Book Synopsis Performance of Twin Two-dimensional Wedge Nozzles Including Thrust Vectoring and Reversing Effects at Speeds Up to Mach 2.20 by : Francis J. Capone
Download or read book Performance of Twin Two-dimensional Wedge Nozzles Including Thrust Vectoring and Reversing Effects at Speeds Up to Mach 2.20 written by Francis J. Capone and published by . This book was released on 1977 with total page 196 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Performance of Twin-dimensional Wedge Nozzles Including Thrust Vectoring and Reversing Effects at Speeds Up to Mach 2.20 by : Francis J. Capone
Download or read book Performance of Twin-dimensional Wedge Nozzles Including Thrust Vectoring and Reversing Effects at Speeds Up to Mach 2.20 written by Francis J. Capone and published by . This book was released on 1977 with total page 212 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Performance of Five Twin-engine Nonaxisymmetric Nozzles with Vectoring and Reversing Capability by : Francis J. Capone
Download or read book Static Performance of Five Twin-engine Nonaxisymmetric Nozzles with Vectoring and Reversing Capability written by Francis J. Capone and published by . This book was released on 1978 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1986 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Performance of an Isolated Two-dimensional Variable-geometry Wedge Nozzle with Translating Shroud and Collapsing Wedge at Speeds Up to Mach 2.01 by : Donald L. Maiden
Download or read book Performance of an Isolated Two-dimensional Variable-geometry Wedge Nozzle with Translating Shroud and Collapsing Wedge at Speeds Up to Mach 2.01 written by Donald L. Maiden and published by . This book was released on 1975 with total page 75 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind-tunnel investigation was conducted to determine the aeropropulsion performance (thrust-minus-drag) of a single-engine, variable-geometry, two-dimensional (2-D) wedge nozzle with simulated translating-shroud and collapsing-wedge mechanisms. The investigation was conducted statically and at Mach numbers from 0.60 to 2.01 at an angle of attack of 0 deg and at varied jet total-pressure ratios up to 21, depending on the Mach number. The results indicate that the isolated aeropropulsion performance of a variable-geometry two-dimensional wedge nozzle is competitive with axisymmetric nozzles at transonic and supersonic speeds, but the isolated performance is slightly inferior for static take-off and low subsonic speeds. With the use of a simple tertiary-air ejector, the static take-off performance was increased.
Book Synopsis Static Internal Performance Including Thrust Vectoring and Reversing of Two-dimensional Convergent-divergent Nozzles by :
Download or read book Static Internal Performance Including Thrust Vectoring and Reversing of Two-dimensional Convergent-divergent Nozzles written by and published by . This book was released on 1984 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Internal Performance of a Thrust Vectoring and Reversing Two-dimensional Convergent-divergent Nozzle with an Aft Flap by : Richard J. Re
Download or read book Static Internal Performance of a Thrust Vectoring and Reversing Two-dimensional Convergent-divergent Nozzle with an Aft Flap written by Richard J. Re and published by . This book was released on 1986 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pitot-pressure Measurements in Flow Fields Behind a Rectangular Nozzle with Exhaust Jet for Free-stream Mach Numbers of 0.00, 0.60, and 1.20 by : Lawrence Elwood Putnam
Download or read book Pitot-pressure Measurements in Flow Fields Behind a Rectangular Nozzle with Exhaust Jet for Free-stream Mach Numbers of 0.00, 0.60, and 1.20 written by Lawrence Elwood Putnam and published by . This book was released on 1986 with total page 160 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Internal Performance of a Thrust Vectoring and Reversing Two-dimensional Convergent-divergent Nozzle with an Aft Flap by : Richard J. Re
Download or read book Static Internal Performance of a Thrust Vectoring and Reversing Two-dimensional Convergent-divergent Nozzle with an Aft Flap written by Richard J. Re and published by . This book was released on 1986 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Internal Performance Including Thrust Vectoring and Reversing of Tow-dimensional Convergent-divergent Nozzles by : Richard J. Re
Download or read book Static Internal Performance Including Thrust Vectoring and Reversing of Tow-dimensional Convergent-divergent Nozzles written by Richard J. Re and published by . This book was released on 1984 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pilot-pressure Measurements in Flow Fields Behind a Rectangular Nozzle with Exhaust Jet for Free-stream Mach Numbers of 0.00, 0.60, and 1.20 by :
Download or read book Pilot-pressure Measurements in Flow Fields Behind a Rectangular Nozzle with Exhaust Jet for Free-stream Mach Numbers of 0.00, 0.60, and 1.20 written by and published by . This book was released on 1986 with total page 160 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Internal Pressure Distributions for a Two-dimensional Thrust-reversing Nozzle Operating at a Free-stream Mach Number of Zero by : Lawrence Elwood Putnam
Download or read book Internal Pressure Distributions for a Two-dimensional Thrust-reversing Nozzle Operating at a Free-stream Mach Number of Zero written by Lawrence Elwood Putnam and published by . This book was released on 1983 with total page 50 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 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:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722771683 Total Pages :82 pages Book Rating :4.7/5 (716 download)
Book Synopsis Static Performance of a Cruciform Nozzle with Multiaxis Thrust-Vectoring and Reverse-Thrust Capabilities by : National Aeronautics and Space Administration (NASA)
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...
Book Synopsis Static Internal Performance Characteristics of Two Thrust-reverser Concepts for Axisymmetric Nozzles by : Laurence D. Leavitt
Download or read book Static Internal Performance Characteristics of Two Thrust-reverser Concepts for Axisymmetric Nozzles written by Laurence D. Leavitt and published by . This book was released on 1982 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of Thrust Vectoring Two-dimensional Convergent-divergent Nozzles Installed in a Twin-engine Fighter Model at High Angles of Attack by :
Download or read book An Experimental Investigation of Thrust Vectoring Two-dimensional Convergent-divergent Nozzles Installed in a Twin-engine Fighter Model at High Angles of Attack written by and published by . This book was released on 1990 with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt:
