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Divergence Thrust Loss Calculations For Convergent Divergent Nozzles
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781725722637 Total Pages :34 pages Book Rating :4.7/5 (226 download)
Book Synopsis Divergence Thrust Loss Calculations for Convergent-Divergent Nozzles by : National Aeronautics and Space Administration (NASA)
Download or read book Divergence Thrust Loss Calculations for Convergent-Divergent Nozzles written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-17 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: The analytical derivations of the non-axial thrust divergence losses for convergent-divergent nozzles are described as well as how these calculations are embodied in the Navy/NASA engine computer program. The convergent-divergent geometries considered are simple classic axisymmetric nozzles, two dimensional rectangular nozzles, and axisymmetric and two dimensional plug nozzles. A simple, traditional, inviscid mathematical approach is used to deduce the influence of the ineffectual non-axial thrust as a function of the nozzle exit divergence angle. Berton, Jeffrey J. Glenn Research Center NASA-TM-105176, E-6472, NAS 1.15:105176 RTOP 537-01-22...
Book Synopsis Divergence Thrust Loss Calculations for Convergent-divergent Nozzles: Extensions to the Classical Case by :
Download or read book Divergence Thrust Loss Calculations for Convergent-divergent Nozzles: Extensions to the Classical Case written by and published by . This book was released on 1991 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Book Synopsis Internal Performance of Several Divergent-shroud Ejector Nozzles with High Divergence Angles by : Arthur M. Trout
Download or read book Internal Performance of Several Divergent-shroud Ejector Nozzles with High Divergence Angles written by Arthur M. Trout and published by . This book was released on 1957 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Convergent-divergent Nozzles Applicable to Reduced-power Supersonic Cruise Aircraft by : Booby L. Berrier
Download or read book Investigation of Convergent-divergent Nozzles Applicable to Reduced-power Supersonic Cruise Aircraft written by Booby L. Berrier and published by . This book was released on 1980 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Book Synopsis Static Investigation of a Two-dimensional Convergent-divergent Exhaust Nozzle with Multiaxis Thrust-vectoring Capability by : John Gordon Taylor
Download or read book Static Investigation of a Two-dimensional Convergent-divergent Exhaust Nozzle with Multiaxis Thrust-vectoring Capability written by John Gordon Taylor and published by . This book was released on 1990 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 1991 with total page 1460 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.
Book Synopsis The Influence of Design Pressure Ratio and Divergence Angle on the Thrust of Convergent-divergent Propelling Nozzles by : Aeronautical Research Council
Download or read book The Influence of Design Pressure Ratio and Divergence Angle on the Thrust of Convergent-divergent Propelling Nozzles written by Aeronautical Research Council and published by . This book was released on 1957 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Influence of Design Pressure Ratio and Divergence Angle on the Thrust of Convergent-divergent Propelling Nozzles by : P. F. Ashwood
Download or read book The Influence of Design Pressure Ratio and Divergence Angle on the Thrust of Convergent-divergent Propelling Nozzles written by P. F. Ashwood and published by . This book was released on 1957 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Cold-air Investigation of Three Variable-throat-area Convergent-divergent Nozzles by : John E. McAulay
Download or read book Cold-air Investigation of Three Variable-throat-area Convergent-divergent Nozzles written by John E. McAulay and published by . This book was released on 1959 with total page 36 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 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 The Influence of Design Pressure Ratio and Divergence Angle on the Thrust of Convergent-divergent Propelling Nozzles by : P. F. Ashwood
Download or read book The Influence of Design Pressure Ratio and Divergence Angle on the Thrust of Convergent-divergent Propelling Nozzles written by P. F. Ashwood and published by . This book was released on 1955 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Internal Performance of a Two-dimensional Convergent-divergent Nozzle with Thrust Vectoring by : E. Ann Bare
Download or read book Static Internal Performance of a Two-dimensional Convergent-divergent Nozzle with Thrust Vectoring written by E. Ann Bare and published by . This book was released on 1987 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Thrust Coefficients of Low-thrust Nozzles by : Ernie W. Spisz
Download or read book Thrust Coefficients of Low-thrust Nozzles written by Ernie W. Spisz and published by . This book was released on 1965 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: The performance losses associated with small nozzles operating at low propellant flow rates were investigated experimentally with a resistance-heated hydrogen thrustor. Data were obtained for seven different nozzles covering the range of nozzle area ratio from 25 to 150, hydrogen propellant flow rates of 0.5x10 to the -4, 1.0x10 to the -4, and 2.5x10 to the -4 pound per second, and propellant temperatures from 530 to 4000 R. The nozzle losses, as determined by the difference between the one-dimensional isentropic thrust coefficient and the measured thrust coefficient, were correlated in terms of the throat Reynolds number and nozzle area ratio. At low throat Reynolds number, the nozzle losses were sufficiently large to result in measured thrust coefficients less than the values calculated for isentropic flow through a choked orifice. Results show that large area ratios are not required for achieving maximum thrust for nozzles with low throat Reynolds number (
Book Synopsis Measurements of Thrust from Convergent-divergent Propelling Nozzles by : P. J. Fletcher
Download or read book Measurements of Thrust from Convergent-divergent Propelling Nozzles written by P. J. Fletcher and published by . This book was released on 1952 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt:
