Two-dimensional Converging-diverging Rippled Nozzles at Transonic Speeds

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ISBN 13 :
Total Pages : 116 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Two-dimensional Converging-diverging Rippled Nozzles at Transonic Speeds by : John R. Carlson

Download or read book Two-dimensional Converging-diverging Rippled Nozzles at Transonic Speeds written by John R. Carlson and published by . This book was released on 1994 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Two-Dimensional Converging-Diverging Rippled Nozzles at Transonic Speeds. Performed in the Langley 16-Foot Transonic Tunnel

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781723469879
Total Pages : 112 pages
Book Rating : 4.4/5 (698 download)

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Book Synopsis Two-Dimensional Converging-Diverging Rippled Nozzles at Transonic Speeds. Performed in the Langley 16-Foot Transonic Tunnel by : National Aeronautics and Space Administration (NASA)

Download or read book Two-Dimensional Converging-Diverging Rippled Nozzles at Transonic Speeds. Performed in the Langley 16-Foot Transonic Tunnel written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-23 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was performed in the Langley 16-Foot Transonic tunnel to determine the effects of external and internal flap rippling on the aerodynamics of a nonaxisymmetric nozzle. Data were obtained at several Mach numbers from static conditions to 1.2 over a range of nozzle pressure ratios. Nozzles with chordal boattail angles of 10, 20, and 30 degrees, with and without surface rippling, were tested. No effect on discharge coefficient due to surface rippling was observed. Internal thrust losses due to surface rippling were measured and attributed to a combination of additional internal skin friction and shock losses. External nozzle drag for the baseline configurations were generally less than that for the rippled configurations at all free-stream Mach numbers tested. The difference between the baseline and rippled nozzle drag levels generally increased with increasing boat tail angle. The thrust-minus-drag level for each rippled nozzle configuration was less than the equivalent baseline configuration for each Mach number at the design nozzle pressure ratio. Carlson, John R. and Asbury, Scott C. Langley Research Center CONVERGENT-DIVERGENT NOZZLES; DISCHARGE COEFFICIENT; DRAG; NOZZLE FLOW; NOZZLE GEOMETRY; THRUST; TRAILING EDGES; TRANSONIC SPEED; WIND TUNNEL TESTS; ANGLE OF ATTACK; BOATTAILS; INTERNAL FRICTION; MACH NUMBER; PRESSURE RATIO; SEPARATED FLOW; SKIN FRICTION...

Monthly Catalog of United States Government Publications

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ISBN 13 :
Total Pages : 1032 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis Monthly Catalog of United States Government Publications by :

Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1995 with total page 1032 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 704 pages
Book Rating : 4.:/5 (31 download)

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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 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalogue, United States Public Documents

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ISBN 13 :
Total Pages : 1638 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Monthly Catalogue, United States Public Documents by :

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:

First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop

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ISBN 13 :
Total Pages : 354 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop by : Richard M. Wood

Download or read book First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop written by Richard M. Wood and published by . This book was released on 1999 with total page 354 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Memorandum

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ISBN 13 :
Total Pages : 182 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis NASA Technical Memorandum by :

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1963 with total page 182 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Effect of Throat Contouring on Two-dimensional Converging-diverging Nozzles at Static Conditions

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ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis The Effect of Throat Contouring on Two-dimensional Converging-diverging Nozzles at Static Conditions by : Mary L. Mason

Download or read book The Effect of Throat Contouring on Two-dimensional Converging-diverging Nozzles at Static Conditions written by Mary L. Mason and published by . This book was released on 1980 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Effect of Throat Contouring on Two-dimensional Converging-diverging Nozzles at Static Conditions

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ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis The Effect of Throat Contouring on Two-dimensional Converging-diverging Nozzles at Static Conditions by : Mary L. Mason

Download or read book The Effect of Throat Contouring on Two-dimensional Converging-diverging Nozzles at Static Conditions written by Mary L. Mason and published by . This book was released on 1980 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Paper

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ISBN 13 :
Total Pages : 116 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis NASA Technical Paper by :

Download or read book NASA Technical Paper written by and published by . This book was released on 1994 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The NASA Langley 16-foot Transonic Tunnel: Historical Overview, Facility Description, Calibration, Flow Characteristics, and Test Capabilities

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ISBN 13 :
Total Pages : 208 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis The NASA Langley 16-foot Transonic Tunnel: Historical Overview, Facility Description, Calibration, Flow Characteristics, and Test Capabilities by : Francis J. Capone

Download or read book The NASA Langley 16-foot Transonic Tunnel: Historical Overview, Facility Description, Calibration, Flow Characteristics, and Test Capabilities written by Francis J. Capone and published by . This book was released on 1995 with total page 208 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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

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Publisher :
ISBN 13 :
Total Pages : 470 pages
Book Rating : 4.:/5 (317 download)

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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:

Transonic Performance of Two Convergent-divergent Ejector Nozzles Designed for Corrected Secondary Flow of 3 and 9.4 Percent

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ISBN 13 :
Total Pages : 78 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Transonic Performance of Two Convergent-divergent Ejector Nozzles Designed for Corrected Secondary Flow of 3 and 9.4 Percent by :

Download or read book Transonic Performance of Two Convergent-divergent Ejector Nozzles Designed for Corrected Secondary Flow of 3 and 9.4 Percent written by and published by . This book was released on 1964 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Langley Scientific and Technical Information Output: 1994, Volume 1

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ISBN 13 :
Total Pages : 180 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis NASA Langley Scientific and Technical Information Output: 1994, Volume 1 by :

Download or read book NASA Langley Scientific and Technical Information Output: 1994, Volume 1 written by and published by . This book was released on 1995 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:

33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit

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ISBN 13 :
Total Pages : 622 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit by :

Download or read book 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit written by and published by . This book was released on 1997 with total page 622 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Comparison of Transonic Flow Solutions in C-D Nozzles

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ISBN 13 :
Total Pages : 99 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Comparison of Transonic Flow Solutions in C-D Nozzles by : Robert J Mary (Jr)

Download or read book Comparison of Transonic Flow Solutions in C-D Nozzles written by Robert J Mary (Jr) and published by . This book was released on 1974 with total page 99 pages. Available in PDF, EPUB and Kindle. Book excerpt: The method of characteristics has proven to be a highly accurate and relatively straight forward technique for computing the supersonic flow field in a two-dimensional or axisymmetric nozzle. However, the method of characteristics requires an initial value line traversing the flow in the fully supersonic region on which the flow properties are known. A parametric study of the effect of different transonic flow calculation methods for establishing the initial value line for axisymmetric converging-diverging nozzles was conducted. The Mach number and radial velocity distributions along a reference start line were calculated and compared for several different transonic solutions for a series of nozzles with different throat radii of curvature. These initial value lines were then used to initiate a method of characteristics analysis of several geometrically different axisymmetric nozzles in order to investigate the impact on calculated performance.

Government Reports Announcements & Index

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ISBN 13 :
Total Pages : 804 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Government Reports Announcements & Index by :

Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1995 with total page 804 pages. Available in PDF, EPUB and Kindle. Book excerpt: