One-Dimensional Gas Flow through the Rocket Motor Nozzle
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F11%3A00442111" target="_blank" >RIV/60162694:G43__/11:00442111 - isvavai.cz</a>
Result on the web
<a href="http://vavtest.unob.cz/registr" target="_blank" >http://vavtest.unob.cz/registr</a>
DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
One-Dimensional Gas Flow through the Rocket Motor Nozzle
Original language description
The paper deals with a solution of possible theoretical regimes of a gas flow through a rocket motor geometric nozzle under conditions of back pressure changes acting against the main gas flow in the nozzle. The numerical solution of basic equations of the gas flow utilizes the Finite Volume Method. The results of solution are compared with the isentropic flow through the same shape of nozzle.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
KA - Militarism
OECD FORD branch
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Result continuities
Project
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Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Others
Publication year
2011
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
International Conference on Military Technology.
ISBN
978-80-7231-787-5
ISSN
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e-ISSN
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Number of pages
7
Pages from-to
479-485
Publisher name
Univerzita obrany, Brno
Place of publication
Brno
Event location
BVV Trade Fairs, Brno, Czech Republic
Event date
May 10, 2011
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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