Flow Field Analysis of a Nozzle-Boattail System

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ISBN 13 :
Total Pages : 114 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Flow Field Analysis of a Nozzle-Boattail System by : Stephen A. Pasley

Download or read book Flow Field Analysis of a Nozzle-Boattail System written by Stephen A. Pasley and published by . This book was released on 1974 with total page 114 pages. Available in PDF, EPUB and Kindle. Book excerpt: A production type computer program has been developed which is capable of analyzing the supersonic flow fields associated with aximmetric nozzle-base-boattail assemblies. Using the method of characteristics, an analysis for both the nozzle and boattail flow fields was developed. The analysis is based on the governing gas dynamic equations for a rotational flow of a frozen or equilibrium gas mixture. The transonic method developed by Kliegel was used to obtain the initial-value line for the nozzle flow field analysis. If desired, axisymmetric tabular data can be input for the nozzle initial-value line. Either uniform flow or axisymmetric tabular data can be used to specify the initial-value line for the boattail flow field analysis. The nozzle and boattail contours can be specified as conical, second-order polynomial or tabular contours. (Author).

Investigations of a Flow Field Surrounding Circular-arc Boattail Nozzles at Subsonic Speeds

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ISBN 13 :
Total Pages : 164 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Investigations of a Flow Field Surrounding Circular-arc Boattail Nozzles at Subsonic Speeds by : William Kelly Abeyounis

Download or read book Investigations of a Flow Field Surrounding Circular-arc Boattail Nozzles at Subsonic Speeds written by William Kelly Abeyounis and published by . This book was released on 1980 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Improved Analytical Model of the Separation Region on Boattail Nozzles at Subsonic Speeds

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ISBN 13 :
Total Pages : 92 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis An Improved Analytical Model of the Separation Region on Boattail Nozzles at Subsonic Speeds by : Walter M. Presz

Download or read book An Improved Analytical Model of the Separation Region on Boattail Nozzles at Subsonic Speeds written by Walter M. Presz and published by . This book was released on 1978 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 1126 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 1987 with total page 1126 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.

Masters Theses in the Pure and Applied Sciences

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Publisher : Springer Science & Business Media
ISBN 13 : 147575776X
Total Pages : 299 pages
Book Rating : 4.4/5 (757 download)

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Book Synopsis Masters Theses in the Pure and Applied Sciences by : Wade H. Shafer

Download or read book Masters Theses in the Pure and Applied Sciences written by Wade H. Shafer and published by Springer Science & Business Media. This book was released on 2013-12-11 with total page 299 pages. Available in PDF, EPUB and Kindle. Book excerpt: Masters Theses in the Pure and Applied Sciences was first conceived, published, and dis seminated by the Center for Information and Numerical Data Analysis and Synthesis, (CINDAS) *at Purdue University in 1957, starting its coverage of theses with the academic year 1955. Beginning with Volume 13, the printing and dissemination phases of the ac tivity was transferred to University Microfilms/Xerox of Ann Arbor, Michigan, with the thought that such an arrangement would be more beneficial to the academic and general scientific and technical community. After five years of this joint undertaking we had concluded that it was in the interest of all concerned if the printing and distribution of the volume were handled by an international publishing house to assure improved service and broader dissemination. Hence, starting with Volume 18, Masters Theses in the Pure and Applied Sciences has been disseminated on a worldwide basis by Plenum Publishing Corporation of New York, and in the same year the coverage was broadened to include Canadian universities. All back issues can also be ordered from Plenum. We have reported in Volume 19 (thesis year 1974) a total of 10,045 theses titles from 20 Canadian and 209 United States universities. We are sure that this broader base for theses titles reported will greatly enhance the value of this important annual reference work. The organization of Volume 19 is identical to that of past years. It consists of theses titles arranged by discipline and by university within each discipline.

Analytical and Experimental Study of Axisymmetric Truncated Plug Nozzle Flow Fields

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ISBN 13 :
Total Pages : 138 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Analytical and Experimental Study of Axisymmetric Truncated Plug Nozzle Flow Fields by : T. J. Mueller

Download or read book Analytical and Experimental Study of Axisymmetric Truncated Plug Nozzle Flow Fields written by T. J. Mueller and published by . This book was released on 1972 with total page 138 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Investigations of a Flow Field Surrounding Circular-arc Boattail Nozzles at Subsonic Speeds

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Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (761 download)

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Book Synopsis Investigations of a Flow Field Surrounding Circular-arc Boattail Nozzles at Subsonic Speeds by : William Kelly Abeyounis

Download or read book Investigations of a Flow Field Surrounding Circular-arc Boattail Nozzles at Subsonic Speeds written by William Kelly Abeyounis and published by . This book was released on 1980 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flow Analysis of Nozzle Installations with Strong Airplane Flow Interactions

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ISBN 13 :
Total Pages : 72 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Flow Analysis of Nozzle Installations with Strong Airplane Flow Interactions by :

Download or read book Flow Analysis of Nozzle Installations with Strong Airplane Flow Interactions written by and published by . This book was released on 1982 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Inventory of Energy Research and Development, 1973-1975

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ISBN 13 :
Total Pages : 1458 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Inventory of Energy Research and Development, 1973-1975 by : Oak Ridge National Laboratory

Download or read book Inventory of Energy Research and Development, 1973-1975 written by Oak Ridge National Laboratory and published by . This book was released on 1976 with total page 1458 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Investigation of Nozzle External Flow

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ISBN 13 :
Total Pages : 88 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Investigation of Nozzle External Flow by : Sergio Panunzio

Download or read book Investigation of Nozzle External Flow written by Sergio Panunzio and published by . This book was released on 1976 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of an experimental investigation of the transonic flow over a turbojet boat-tail including the effects of the nozzle exhaust flow are presented. A new type of transonic facility with controllable infection and porosity at the tunnel wall was developed. It was used in the present investigation to simulate accurately both the inviscid and viscous flow fields so as to best represent the complex interaction prevalent at these conditions. The operation and performance of the facility is described here. The AGARD 15 degrees boat-tail nozzle was used in the present study since the flow field over this nacelle has been reported extensively by several investigators. Therefore it established a reference configuration that serves to check proper facility operation and for comparison of the results. The present tests were conducted at a Mach number of approximately .90 in a test section of 23.25 inch (59.0 cm) diameter. Detailed measurements of the static pressure distribution on the boat-tail in the facility indicate a significant upstream movement of the separation point and shock with small to moderate changes in the nozzle pressure ratio while increases in the Reynolds number cause a downstream movement of the separation point and of the shock wave.

Propulsion Nozzle Studies

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

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Book Synopsis Propulsion Nozzle Studies by :

Download or read book Propulsion Nozzle Studies written by and published by . This book was released on 1976 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Propulsion Nozzle Studies. Volume II. Design of Maximum Thrust Nozzle-Base-Boattail Contours

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ISBN 13 :
Total Pages : 122 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Propulsion Nozzle Studies. Volume II. Design of Maximum Thrust Nozzle-Base-Boattail Contours by : Jeffrey G. Allman

Download or read book Propulsion Nozzle Studies. Volume II. Design of Maximum Thrust Nozzle-Base-Boattail Contours written by Jeffrey G. Allman and published by . This book was released on 1977 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt: A production-type computer program was developed for the design of maximum thrust axisymmetric nozzle-base-boattail contours. The flow field analysis is based on the governing equations for the rotational flow of a frozen or equilibrium gas mixture. The contour optimization is based on the direct optimization of a nonlinear function of several (three or less) geometric variables. The nozzle and boattail contours are modeled as a second-order polynomial and a cone, respectively. For fixed initial contours and nozzle and boattail lengths, the second-order polynomial nozzle contour is uniquely specified by the nozzle throat attachment angle and the nozzle exit lip radius, and the conical boattail is uniquely specified by the boattail exit lip radius. These three independent parameters are varied to determine the unique nozzle-base-boattail configuration that yields maximum thrust. Three methods are included in the program to determine the maximum thrust contour. Each method requires an initial estimate of the geometry that produces maximum thrust. The three methods were also applied to the design of nozzle-base-boattail configurations. The three-dimensional optimizations were found to be practical for finding the maximum thrust attainable for a nozzle-base-boattail assembly. Each of the three methods converged efficiently to the maximum thrust nozzle-base-boattail contour.

An Evaluation of Nozzle Afterbody Code

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ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis An Evaluation of Nozzle Afterbody Code by : Frederick C. Guyton

Download or read book An Evaluation of Nozzle Afterbody Code written by Frederick C. Guyton and published by . This book was released on 1986 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Frontiers of Computational Fluid Dynamics 2002

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Publisher : World Scientific
ISBN 13 : 9810248490
Total Pages : 523 pages
Book Rating : 4.8/5 (12 download)

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Book Synopsis Frontiers of Computational Fluid Dynamics 2002 by : David A. Caughey

Download or read book Frontiers of Computational Fluid Dynamics 2002 written by David A. Caughey and published by World Scientific. This book was released on 2002 with total page 523 pages. Available in PDF, EPUB and Kindle. Book excerpt: This series of volumes on the ?Frontiers of Computational Fluid Dynamics? was introduced to honor contributors who have made a major impact on the field. The first volume was published in 1994 and was dedicated to Prof Antony Jameson; the second was published in 1998 and was dedicated to Prof Earl Murman. The volume is dedicated to Prof Robert MacCormack.The twenty-six chapters in the current volume have been written by leading researchers from academia, government laboratories, and industry. They present up-to-date descriptions of recent developments in techniques for numerical analysis of fluid flow problems, and applications of these techniques to important problems in industry, as well as the classic paper that introduced the ?MacCormack scheme? to the world.

A Time-dependent Analysis for Quasi-one-dimensional Nozzle Flows with Vibrational and Chemical Nonequilibrium

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ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis A Time-dependent Analysis for Quasi-one-dimensional Nozzle Flows with Vibrational and Chemical Nonequilibrium by : John David Anderson (Jr.)

Download or read book A Time-dependent Analysis for Quasi-one-dimensional Nozzle Flows with Vibrational and Chemical Nonequilibrium written by John David Anderson (Jr.) and published by . This book was released on 1969 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: A new technique is presented for the numerical solution of quasi-one-dimensional, vibrational and chemical nonequilibrium nozzle flows including nonequilibrium conditions both upstream and downstream of the throat. This new technique is a time-dependent analysis which entails the explicite finite-difference solution of the quasi-one-dimensional unsteady flow equations in steps of time, starting with assumed initial distributions throughout the nozzle. The steady-state solution is approached at large values of time. A virtue of the present time-dependent analysis is its simplicity, which prevails from its initial physical formulation to the successful receipt of numerical results. Also, the present solution yields the transient as well as the steady-state nonequilibrium nozzle flows. To exemplify the present analysis, results are given for several cases of vibrational and chemical nonequilibrium expansions through nozzles. (Author).

Government Reports Annual Index

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ISBN 13 :
Total Pages : 882 pages
Book Rating : 4.:/5 (3 download)

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Book Synopsis Government Reports Annual Index by :

Download or read book Government Reports Annual Index written by and published by . This book was released on 1975 with total page 882 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Reference Publication

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ISBN 13 :
Total Pages : 116 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis NASA Reference Publication by :

Download or read book NASA Reference Publication written by and published by . This book was released on 1977 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt: