An Approximate Theoretical Method for Modeling the Static Thrust Performance of Non-axisymmetric Two-dimensional Convergent-divergent Nozzles

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Total Pages : 54 pages
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Book Synopsis An Approximate Theoretical Method for Modeling the Static Thrust Performance of Non-axisymmetric Two-dimensional Convergent-divergent Nozzles by :

Download or read book An Approximate Theoretical Method for Modeling the Static Thrust Performance of Non-axisymmetric Two-dimensional Convergent-divergent Nozzles written by and published by . This book was released on 1995 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 488 pages
Book Rating : 4.:/5 (3 download)

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Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 488 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Monthly Catalogue, United States Public Documents

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Total Pages : 1638 pages
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Download or read book Monthly Catalogue, United States Public Documents written by and published by . This book was released on 1995 with total page 1638 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Static Performance of a Fixed-Geometry Exhaust Nozzle Incorporating Porous Cavities for Shock-Boundary Layer Interaction Control

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Total Pages : 142 pages
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Book Synopsis Static Performance of a Fixed-Geometry Exhaust Nozzle Incorporating Porous Cavities for Shock-Boundary Layer Interaction Control by : Scott C. Asbury

Download or read book Static Performance of a Fixed-Geometry Exhaust Nozzle Incorporating Porous Cavities for Shock-Boundary Layer Interaction Control written by Scott C. Asbury and published by . This book was released on 1999 with total page 142 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Paper

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Total Pages : 154 pages
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Download or read book NASA Technical Paper written by and published by . This book was released on 1997 with total page 154 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalog of United States Government Publications

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ISBN 13 :
Total Pages : 800 pages
Book Rating : 4.3/5 (243 download)

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Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1983 with total page 800 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Convoluted Divergent Flap Contouring on the Performance of a Fixed-Geometry Nonaxisymmetric Exhaust Nozzle

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Total Pages : 78 pages
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Book Synopsis Effects of Convoluted Divergent Flap Contouring on the Performance of a Fixed-Geometry Nonaxisymmetric Exhaust Nozzle by : Scott C. Asbury

Download or read book Effects of Convoluted Divergent Flap Contouring on the Performance of a Fixed-Geometry Nonaxisymmetric Exhaust Nozzle written by Scott C. Asbury and published by . This book was released on 1999 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit

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ISBN 13 :
Total Pages : 636 pages
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Book Synopsis 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit by :

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Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 325)

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ISBN 13 :
Total Pages : 470 pages
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Book Synopsis Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 325) by :

Download or read book Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 325) written by and published by . This book was released on 1995 with total page 470 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Static Investigation of a Multiaxis Thrust-Vectoring Nozzle With Variable Internal Contouring Ability

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Total Pages : 154 pages
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Book Synopsis Static Investigation of a Multiaxis Thrust-Vectoring Nozzle With Variable Internal Contouring Ability by : David J. Wing

Download or read book Static Investigation of a Multiaxis Thrust-Vectoring Nozzle With Variable Internal Contouring Ability written by David J. Wing and published by . This book was released on 1997 with total page 154 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Applied Mechanics Reviews

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ISBN 13 :
Total Pages : 840 pages
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Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1979 with total page 840 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Government Reports Announcements & Index

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ISBN 13 :
Total Pages : 458 pages
Book Rating : 4.3/5 (129 download)

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Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1995 with total page 458 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Static Thrust-vectoring Performance of Nonaxisymmetric Convergent-divergent Nozzles with Post-exit Yaw Vanes

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ISBN 13 :
Total Pages : 88 pages
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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:

Thrust Performance of a Variable-geometry, Nonaxisymmetric, Two-dimensional, Convergent-divergent Exhaust Nozzle on a Turbojet Engine at Altitude

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Total Pages : 44 pages
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Book Synopsis Thrust Performance of a Variable-geometry, Nonaxisymmetric, Two-dimensional, Convergent-divergent Exhaust Nozzle on a Turbojet Engine at Altitude by : David M. Straight

Download or read book Thrust Performance of a Variable-geometry, Nonaxisymmetric, Two-dimensional, Convergent-divergent Exhaust Nozzle on a Turbojet Engine at Altitude written by David M. Straight and published by . This book was released on 1983 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Internal Performance of a Hybrid Axisymmetric/nonaxisymmetric Convergent-divergent Nozzle

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ISBN 13 :
Total Pages : 64 pages
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Book Synopsis Internal Performance of a Hybrid Axisymmetric/nonaxisymmetric Convergent-divergent Nozzle by : John G. Taylor

Download or read book Internal Performance of a Hybrid Axisymmetric/nonaxisymmetric Convergent-divergent Nozzle written by John G. Taylor and published by . This book was released on 1991 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Static Performance of Nonaxisymmetric Nozzles with Yaw Thrust-Vectoring Vanes

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722772338
Total Pages : 76 pages
Book Rating : 4.7/5 (723 download)

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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...

NASA Scientific and Technical Publications

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ISBN 13 :
Total Pages : 410 pages
Book Rating : 4.F/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 1987 with total page 410 pages. Available in PDF, EPUB and Kindle. Book excerpt: