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100%: STRAUB: Thermofluiddynamics of Optimized Rocket Propulsions: Extended Lewis Code Fundamentals (ISBN: 9783764323141) Birkhauser Verlag AG 0, Erstausgabe, in Englisch, Broschiert.
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89%: Didier Astruc: Thermofluiddynamics of Optimized Rocket Propulsions : Extended Lewis Code Fundamentals (ISBN: 9783034891509) in Deutsch, auch als eBook.
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88%: Straub, Dieter: Thermofluiddynamics of Optimized Rocket Propulsions: Extended Lewis Code Fundamentals (ISBN: 9780817623142) 1989, in Englisch, Broschiert.
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78%: Prof.D. Straub: Thermofluiddynamics of Optimized Rocket Propulsions: Extended Lewis Code Fundamentals (Paperback) (ISBN: 9783034899277) in Deutsch.
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Thermofluiddynamics of Optimized Rocket Propulsions: Extended Lewis Code Fundamentals
15 Angebote vergleichen
Preise | 2013 | 2015 | 2019 |
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Schnitt | € 442,88 | € 88,49 | € 64,91 |
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Thermofluiddynamics of Optimized Rocket Propulsions: Extended Lewis Code Fundamentals (1998)
DE US FE
ISBN: 9783764323141 bzw. 3764323140, in Deutsch, Birkhäuser, gebraucht, Erstausgabe.
Von Händler/Antiquariat, Better World Books [51315977], Mishawaka, IN, U.S.A.
Former Library book. Shows some signs of wear, and may have some markings on the inside.
Former Library book. Shows some signs of wear, and may have some markings on the inside.
2
Thermofluiddynamics of Optimized Rocket Propulsions
DE
ISBN: 9783764323141 bzw. 3764323140, in Deutsch, Birkhauser.
Lieferung aus: Vereinigte Staaten von Amerika, Lagernd.
Thermofluiddynamics of Optimized Rocket Propulsions Straub / Straub, Dieter, 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.
Thermofluiddynamics of Optimized Rocket Propulsions Straub / Straub, Dieter, 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.
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Thermofluiddynamics of Optimized Rocket Propulsions: Extended Lewis Code Fundamentals
EN HC US
ISBN: 9780817623142 bzw. 0817623140, in Englisch, Birkhauser, gebundenes Buch, gebraucht.
Lieferung aus: Vereinigte Staaten von Amerika, Versandkosten nach: USA.
Von Händler/Antiquariat, Books Express.
Birkhauser. Hardcover. Good. We ship International with Tracking Number! May not contain Access Codes or Supplements. Buy with confidence, excellent customer service! L.
Von Händler/Antiquariat, Books Express.
Birkhauser. Hardcover. Good. We ship International with Tracking Number! May not contain Access Codes or Supplements. Buy with confidence, excellent customer service! L.
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Thermofluiddynamics of Optimized Rocket Propulsions (1989)
EN US
ISBN: 9783764323141 bzw. 3764323140, in Englisch, 265 Seiten, Birkhauser Verlag AG, gebraucht.
Lieferung aus: Frankreich, Expédition sous 1 à 2 jours ouvrés.
Von Händler/Antiquariat, Nearfine.
Die Beschreibung dieses Angebotes ist von geringer Qualität oder in einer Fremdsprache. Trotzdem anzeigen
Von Händler/Antiquariat, Nearfine.
Die Beschreibung dieses Angebotes ist von geringer Qualität oder in einer Fremdsprache. Trotzdem anzeigen
8
Thermofluiddynamics of Optimized Rocket Propulsions
DE NW EB
ISBN: 9783034891509 bzw. 3034891504, in Deutsch, Springer Nature, neu, E-Book.
Lieferung aus: Deutschland, Lagernd, zzgl. Versandkosten.
combustion, design, dynamics, engine, flow, modeling, rocket engine, Engineering; Engineering Fluid Dynamics, eBook.
combustion, design, dynamics, engine, flow, modeling, rocket engine, Engineering; Engineering Fluid Dynamics, eBook.
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Thermofluiddynamics of Optimized Rocket Propulsions Extendedlewis (1989)
EN HC NW
ISBN: 9780817623142 bzw. 0817623140, in Englisch, Birkhauser, gebundenes Buch, neu.
Lieferung aus: Indien, zzgl. Versandkosten, Verandgebiet: INT.
Von Händler/Antiquariat, DELHI BOOK STORE, DELHI, NEW DELHI, [RE:5].
Hard cover, Illustrated.
Von Händler/Antiquariat, DELHI BOOK STORE, DELHI, NEW DELHI, [RE:5].
Hard cover, Illustrated.
10
Thermofluiddynamics of Optimized Rocket Propulsions: Extended Lewis Code Fundamentals (1989)
EN PB US
ISBN: 9783764323141 bzw. 3764323140, in Englisch, 266 Seiten, Birkhäuser, Taschenbuch, gebraucht.
Lieferung aus: Deutschland, Versandfertig in 1 - 2 Werktagen, Versandkostenfrei. Tatsächliche Versandkosten können abweichen.
Von Händler/Antiquariat, Books N planet.
Die Beschreibung dieses Angebotes ist von geringer Qualität oder in einer Fremdsprache. Trotzdem anzeigen
Von Händler/Antiquariat, Books N planet.
Die Beschreibung dieses Angebotes ist von geringer Qualität oder in einer Fremdsprache. Trotzdem anzeigen
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