A Computer Program for the Performance Analysis of Scarfed Nozzles

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ISBN 13 :
Total Pages : 376 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis A Computer Program for the Performance Analysis of Scarfed Nozzles by :

Download or read book A Computer Program for the Performance Analysis of Scarfed Nozzles written by and published by . This book was released on 1984 with total page 376 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analysis is presented for predicting the performance of scarfed propulsive nozzles. The model assumes that the scarfing is not severe, so that the flow within the nozzle is axisymmetric. The flowfield within the nozzle and the scarfed nozzle extension is calculated by the method of characteristics. The oblique shock wave emaninating from the junction of the nozzle and the scarfed nozzle extension is fitted discretely and tracked through the flowfield. The nozzle forces are determined by integrating the wall pressure distribution. Nozzle axial and side forces are calculated, and missile axial and side forces are determined. A computer program implementing the analysis is discussed. Fifteen sample cases are presented to illustrate the use of the computer program.

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 490 pages
Book Rating : 4.:/5 (319 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 1990 with total page 490 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Computer Programme for the Analysis of Nozzle Performance with Or Without Supersonic External Flow

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ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis A Computer Programme for the Analysis of Nozzle Performance with Or Without Supersonic External Flow by : H. J. Willcocks

Download or read book A Computer Programme for the Analysis of Nozzle Performance with Or Without Supersonic External Flow written by H. J. Willcocks and published by . This book was released on 1964 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Analysis and Computer Program for Evaluation of Airbreathing Propulsion Exhaust Nozzle Performance

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ISBN 13 :
Total Pages : 300 pages
Book Rating : 4.:/5 (122 download)

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Book Synopsis Analysis and Computer Program for Evaluation of Airbreathing Propulsion Exhaust Nozzle Performance by : S. Wehofer

Download or read book Analysis and Computer Program for Evaluation of Airbreathing Propulsion Exhaust Nozzle Performance written by S. Wehofer and published by . This book was released on 1973 with total page 300 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analytical technique based on the time-dependent flow equations has been developed to predict the inviscid transonic flow field in axisymmetric propulsion nozzles. The analysis includes the treatment of axisymmetric nonuniform nozzle inlet profiles of total pressure, total temperature, specific heat, and molecular weight. The analysis is also capable of considering convergent-divergent, convergent, and shrouded or unshrouded plug nozzle geometries. A computer listing and three sample calculations are presented to illustrate some of the capabilities of the program. (Author).

Performance Analysis of Compressed Truncated Perfect Nozzles

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ISBN 13 :
Total Pages : 276 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Performance Analysis of Compressed Truncated Perfect Nozzles by : J. D. Hoffman

Download or read book Performance Analysis of Compressed Truncated Perfect Nozzles written by J. D. Hoffman and published by . This book was released on 1984 with total page 276 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analysis is presented for predicting the performance of compressed truncated perfect nozzles. The flowfield within the nozzle is calculated by the method of characteristics. The oblique shock wave formed by the coalescence of right-running Mach lines from the compressed contour is fitted discretely and tracked through the flowfield. The nozzle thrust is determined by integrating the momentum flux and pressure forces across the nozzle throat and integrating the wall pressure forces. A computer program implementing the analysis is discussed. Three sample cases are presented to illustrate the use of the computer program. Additional keywords: models; algorithms; parametric analysis; mathematical prediction. (Author).

85-1301 - AIAA 85-1350

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ISBN 13 :
Total Pages : 482 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis 85-1301 - AIAA 85-1350 by :

Download or read book 85-1301 - AIAA 85-1350 written by and published by . This book was released on 1985 with total page 482 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Papers Presented at the AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference

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ISBN 13 :
Total Pages : 488 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis Papers Presented at the AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference by :

Download or read book Papers Presented at the AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference written by and published by . This book was released on 1989 with total page 488 pages. Available in PDF, EPUB and Kindle. Book excerpt:

AIAA 90-1700 - AIAA 90-1753

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ISBN 13 :
Total Pages : 436 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis AIAA 90-1700 - AIAA 90-1753 by :

Download or read book AIAA 90-1700 - AIAA 90-1753 written by and published by . This book was released on 1990 with total page 436 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Computer Program Abstracts

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ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (3 download)

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Book Synopsis Computer Program Abstracts by :

Download or read book Computer Program Abstracts written by and published by . This book was released on 1972 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Government reports annual index

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ISBN 13 :
Total Pages : 1228 pages
Book Rating : 4.3/5 (129 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 199? with total page 1228 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Applied Mechanics Reviews

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ISBN 13 :
Total Pages : 934 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Applied Mechanics Reviews by :

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1987 with total page 934 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Performance Analysis of an Axisymmetric Thrust-vectoring Nozzle by Using the FUNSIF3-D Code

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Performance Analysis of an Axisymmetric Thrust-vectoring Nozzle by Using the FUNSIF3-D Code by : A. Matesanz

Download or read book Performance Analysis of an Axisymmetric Thrust-vectoring Nozzle by Using the FUNSIF3-D Code written by A. Matesanz and published by . This book was released on 1995 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Reports Awareness Circular : TRAC.

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ISBN 13 :
Total Pages : 520 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Technical Reports Awareness Circular : TRAC. by :

Download or read book Technical Reports Awareness Circular : TRAC. written by and published by . This book was released on 1987 with total page 520 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Nuclear Thermal Rocket Nozzle Testing and Evaluation Program

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ISBN 13 :
Total Pages : 12 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Nuclear Thermal Rocket Nozzle Testing and Evaluation Program by :

Download or read book Nuclear Thermal Rocket Nozzle Testing and Evaluation Program written by and published by . This book was released on 1993 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Fortran Program to Calculate the Flow Field and Performance of an Axially Symmetric DeLaval Nozzle

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

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Book Synopsis A Fortran Program to Calculate the Flow Field and Performance of an Axially Symmetric DeLaval Nozzle by :

Download or read book A Fortran Program to Calculate the Flow Field and Performance of an Axially Symmetric DeLaval Nozzle written by and published by . This book was released on 1965 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Government Reports Announcements & Index

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ISBN 13 :
Total Pages : 1194 pages
Book Rating : 4.0/5 ( 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 1989 with total page 1194 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NPAC-Nozzle Performance Analysis Code

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ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis NPAC-Nozzle Performance Analysis Code by : Paul J. Barnhart

Download or read book NPAC-Nozzle Performance Analysis Code written by Paul J. Barnhart and published by . This book was released on 1997 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: