Performance Of Several Method Of Characteristics Exhaust Nozzles

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Performance of Several Method-of-characteristics Exhaust Nozzles

Author : John M. Farley,Carl E. Campbell
Publisher : Unknown
Page : 38 pages
File Size : 55,5 Mb
Release : 1960
Category : Exhaust nozzles
ISBN : UIUC:30112106588152

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Performance of Several Method-of-characteristics Exhaust Nozzles by John M. Farley,Carl E. Campbell Pdf

Internal Performance Characteristics of Short Convergent-divergent Exhaust Nozzles Designed by the Method of Characteristics

Author : H. George Krull
Publisher : Unknown
Page : 24 pages
File Size : 43,7 Mb
Release : 1956
Category : Charts, diagrams, etc
ISBN : UOM:39015086463919

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Internal Performance Characteristics of Short Convergent-divergent Exhaust Nozzles Designed by the Method of Characteristics by H. George Krull Pdf

An evaluation of the internal performance characteristics of short nozzles designed by the method of characteristics was obtained over a range of nozzle pressure ratios from 1.5 to 22.

Design of Axisymmetric Exhaust Nozzles by Method of Characteristics Incorporating a Variable Isentropic Exponent

Author : Eleanor Costilow Guentert,Harvey E. Neumann
Publisher : Unknown
Page : 28 pages
File Size : 42,6 Mb
Release : 1959
Category : Axial flow
ISBN : NASA:31769000420862

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Design of Axisymmetric Exhaust Nozzles by Method of Characteristics Incorporating a Variable Isentropic Exponent by Eleanor Costilow Guentert,Harvey E. Neumann Pdf

NASA Technical Note

Author : Anonim
Publisher : Unknown
Page : 296 pages
File Size : 49,7 Mb
Release : 1965
Category : Electronic
ISBN : MINN:31951000845935P

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NASA Technical Note by Anonim Pdf

Design of Axisymmetric Exhaust Nozzles by Method of Characteristics Incorporating a Variable Isentropic Exponent

Author : Eleanor Costilow Guentert,Harvey E. Neumann
Publisher : Unknown
Page : 17 pages
File Size : 52,5 Mb
Release : 1959
Category : Electronic
ISBN : OCLC:1070639236

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Design of Axisymmetric Exhaust Nozzles by Method of Characteristics Incorporating a Variable Isentropic Exponent by Eleanor Costilow Guentert,Harvey E. Neumann Pdf

An analytical method for including thermodynamic data with variable isentropic exponent in the method of characteristics as applied to the design of high-temperature exhaust nozzles has been obtained. Several bell-shaped nozzles have been designed with this method. A comparison of nozzle contours obtained by assuming identical boundary conditions and either frozen or equilibrium composition shows that significant differences occur. A computation of the variation of vacuum specific impulse with axial length showed that considerable nozzle length, and hence weight, can be eliminated without serious thrust penalties in nozzle designs that gradually expand the flow to uniform exit conditions.

Index to NASA Technical Publications

Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 128 pages
File Size : 40,7 Mb
Release : 1960-07
Category : Electronic
ISBN : STANFORD:36105024165701

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Index to NASA Technical Publications by United States. National Aeronautics and Space Administration Pdf

Index of N A S A Technical Publications

Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 448 pages
File Size : 44,8 Mb
Release : 1960
Category : Electronic
ISBN : OSU:32435029092020

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Index of N A S A Technical Publications by United States. National Aeronautics and Space Administration Pdf

NASA Technical Paper

Author : Anonim
Publisher : Unknown
Page : 264 pages
File Size : 45,5 Mb
Release : 1991
Category : Science
ISBN : STANFORD:36105024800588

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NASA Technical Paper by Anonim Pdf

Rocket Propulsion Elements

Author : George P. Sutton,Oscar Biblarz
Publisher : John Wiley & Sons
Page : 772 pages
File Size : 54,6 Mb
Release : 2001
Category : Science
ISBN : 0471326429

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Rocket Propulsion Elements by George P. Sutton,Oscar Biblarz Pdf

Aerospace Engineering/Mechanical Engineering The definitive text on rocket propulsion-now completely revised to reflect rapid advancements in the field For more than fifty years, this seminal text has been regarded as the single most authoritative sourcebook on rocket propulsion technology. More comprehensive and coherently organized than any other book on the subject, Rocket Propulsion Elements guides readers evenhandedly through the complex factors that shape propulsion, with both theory and practical design considerations. With more than a third of the text and illustrations either completely new or extensively revised, this latest edition includes current information on engine structures, nozzle theory, gas properties, thrust chambers, launch vehicles, and more. With a detailed table of contents breaking down each chapter into subsections-as well as an expanded index of key words-the Seventh Edition efficiently steers readers quickly to the information they need. Other highlights include: * Separate chapters on liquid, solid, and hybrid propulsion systems and a new chapter on thrust chambers including the new aerospike nozzle * Comprehensive coverage of rocket propulsion technology, with applications to space flight, satellite flight, and guided and unguided missiles * Problem-solving examples and exercises relevant to actual design situations * More than 340 illustrations, including photographs, tables, and graphs * Coherent, up-to-date chapter on electrical propulsion balancing fundamentals with practical aspects and applications For professional engineers in the aerospace and defense industries as well as undergraduate and graduate students in mechanical and aerospace engineering, this time-honored resource is indispensable for its scope of coverage and utility.

NASA Technical Memorandum

Author : Anonim
Publisher : Unknown
Page : 492 pages
File Size : 49,9 Mb
Release : 1994
Category : Aeronautics
ISBN : MINN:31951P00691495X

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NASA Technical Memorandum by Anonim Pdf

Annular Internal-external-expansion Rocket Nozzles for Large Booster Applications

Author : James F. Connors,Robert W. Cubbison,Glenn A. Mitchell
Publisher : Unknown
Page : 36 pages
File Size : 41,6 Mb
Release : 1961
Category : Electronic
ISBN : UIUC:30112106591040

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Annular Internal-external-expansion Rocket Nozzles for Large Booster Applications by James F. Connors,Robert W. Cubbison,Glenn A. Mitchell Pdf

NASA Technical Report

Author : Anonim
Publisher : Unknown
Page : 88 pages
File Size : 44,6 Mb
Release : 1961
Category : Aerodynamics
ISBN : MINN:30000011022112

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NASA Technical Report by Anonim Pdf

Recoilless Rifle Weapon Systems

Author : Nuri Y. Olcer,Sam Lévin
Publisher : Unknown
Page : 556 pages
File Size : 52,9 Mb
Release : 1976
Category : Electronic
ISBN : UIUC:30112101043989

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Recoilless Rifle Weapon Systems by Nuri Y. Olcer,Sam Lévin Pdf