New Design Method of Inlet and Outlet Channels of Turboshaft and Turboprop Engines

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F03%3A00145883" target="_blank" >RIV/68407700:21220/03:00145883 - isvavai.cz</a>
Alternative codes found
RIV/68407700:21260/03:00145883
Result on the web
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DOI - Digital Object Identifier
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Result language
angličtina
Original language name
New Design Method of Inlet and Outlet Channels of Turboshaft and Turboprop Engines
Original language description
New engineering design method for inlet and outlet channels of the turbomachines, casings and ducts of a very complex three dimensional form has been developed at the Department of Aerospace Engineering of the Czech Technical University in Prague. The method was applied for the new design of outlet channel of the Walter M 601 turboprop engine and for the new design of the inlet channel of the Walter M 602 turboprop engine and the regional transport aircraft L 610 with very good results in comparison with the originally designed channels by traditional design methods.
Czech name
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Czech description
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Publication year
2003
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
XVI International Symposium on Air Breathing Engines (ISABE)
ISBN
1-56347-639-8
ISSN
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e-ISSN
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Number of pages
10
Pages from-to
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Publisher name
American Institute of Aeronautics and Astronautics
Place of publication
Reston
Event location
Cleveland, Ohio
Event date
Aug 31, 2003
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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