Author: STRAUB
Publisher: Birkhäuser
ISBN: 3034891504
Category : Technology & Engineering
Languages : en
Pages : 267
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Book Description
This study has two declared aims: it presents the theoretical basis for a provably ideal comparative process for relaxing flows (ICP) and jus tifies its application to jet and, in particular, rocket engines. This will be treated in two parts. Part I offers a status quo report on current calculation methods, and compiles and explains briefly the most important data on selected pro minent rocket engines. Starting from the phenomenology of the dynamical and physico-chemical conversion processes in the fuel-oxidizer fluid mixture and in the burned gases, the ideal thermodynamic comparative process is then derived - as a defined sequential change of states in the system. In order to render this comparative process readily under standable, it is first applied to an appropriate model gas using alge braic equations for all relevant parameters. This model gas undergoes energy conversion processes without forfeiting the simplicity of pre sentation typical of classical gas dynamics. Above all, examination of this model offers proof that it is generally impermissible to use, as is done in practice, the familiar isentropic equation for flow changes of state continuously propagated in flow tube theory. Elementary calculations immediately indicate essential attributes which are also typical for relaxing, multicomponent, one-phase systems, such as the significant 'pressure drop phenomenon' or the establishment of the steady mass flow rate as an 'eigenvalue' of the comparative pro cess. Their relevance to the RE theory is stressed.
Author: STRAUB
Publisher: Birkhäuser
ISBN: 9783764323141
Category : Technology & Engineering
Languages : en
Pages : 266
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Book Description
This study has two declared aims: it presents the theoretical basis for a provably ideal comparative process for relaxing flows (ICP) and jus tifies its application to jet and, in particular, rocket engines. This will be treated in two parts. Part I offers a status quo report on current calculation methods, and compiles and explains briefly the most important data on selected pro minent rocket engines. Starting from the phenomenology of the dynamical and physico-chemical conversion processes in the fuel-oxidizer fluid mixture and in the burned gases, the ideal thermodynamic comparative process is then derived - as a defined sequential change of states in the system. In order to render this comparative process readily under standable, it is first applied to an appropriate model gas using alge braic equations for all relevant parameters. This model gas undergoes energy conversion processes without forfeiting the simplicity of pre sentation typical of classical gas dynamics. Above all, examination of this model offers proof that it is generally impermissible to use, as is done in practice, the familiar isentropic equation for flow changes of state continuously propagated in flow tube theory. Elementary calculations immediately indicate essential attributes which are also typical for relaxing, multicomponent, one-phase systems, such as the significant 'pressure drop phenomenon' or the establishment of the steady mass flow rate as an 'eigenvalue' of the comparative pro cess. Their relevance to the RE theory is stressed.
Author: Dieter Straub
Publisher: Birkhauser
ISBN:
Category : Science
Languages : en
Pages : 280
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Book Description
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 400
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 892
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Book Description
Author:
Publisher:
ISBN:
Category : English imprints
Languages : en
Pages : 1140
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Book Description
Author: New York Public Library
Publisher:
ISBN:
Category : Engineering
Languages : en
Pages : 428
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Book Description
Author: New York Public Library. Research Libraries
Publisher:
ISBN:
Category : Classified catalogs (Universal decimal)
Languages : en
Pages : 848
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Book Description
Author: George Paul Sutton
Publisher: Wiley-Interscience
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 396
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Book Description
A revision of the standard text on the basic technology, performance and design rationale of rocket propulsion. After discussing fundamentals, such as nozzle thermodynamics, heat transfer, flight performance and chemical reaction analysis, the book continues with treatments of various types of liquid and solid propellants and rocket testing. It brings together the engineering science disciplines necessary for rocket design: thermodynamics, heat transfer, flight mechanics, chemical reactions and materials behavior. SI units and information on computer-aided testing have also been added.
Author: D. P. Mishra (Aerospace engineer)
Publisher:
ISBN: 9781523113637
Category : Airplanes
Languages : en
Pages : 461
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Book Description
"The book follows a unified approach to present the basic principles of rocket propulsion in concise and lucid form. This textbook comprises of ten chapters ranging from brief introduction and elements of rocket propulsion, aerothermodynamics to solid, liquid and hybrid propellant rocket engines with chapter on electrical propulsion. Worked out examples are also provided at the end of chapter for understanding uncertainty analysis. This book is designed and developed as an introductory text on the fundamental aspects of rocket propulsion for both undergraduate and graduate students. It is also aimed towards practicing engineers in the field of space engineering. This comprehensive guide also provides adequate problems for audience to understand intricate aspects of rocket propulsion enabling them to design and develop rocket engines for peaceful purposes. Key Features:• Book presents an integrated approach including mechanics, modeling, manufacture and design of composite components including theory and practice.• Exhaustive discussion on analysis and analytical methods for composite beams, columns and plates, and the basic procedure of the finite element method.• Principles of composite manufacturing, common manufacturing methods and selection of manufacturing methods are presented in depth.• Presents concept of design and composite design process, along with several representative design examples.• Includes fully-solved examples with solutions manual and high quality illustrative figures"--Provided by publisher.
