Inlet and Outlet Casings of the Turbojet Engines-Design and Experiment

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F99%3A02012386" target="_blank" >RIV/68407700:21220/99:02012386 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Inlet and Outlet Casings of the Turbojet Engines-Design and Experiment

Original language description

New design method of the 3-D casings of arbitrary shape providing very low total-pressure loss and uniform flow field at inlet or outlet sections of the casings. Application of the method on the design of new inlet and outlet casing for the turboprop engines WALTER.

Czech name

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Czech description

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Type

D - Article in proceedings

CEP classification

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

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Project

<a href="/en/project/OC%20F1.80" target="_blank" >OC F1.80: The regions of concentrated vorticity in a curved cylindrical channel</a><br>

Continuities

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)<br>Z - Vyzkumny zamer (s odkazem do CEZ)

Publication year

1999

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection

First Internat. Confer. on Advanced Engineering Design - Book of Abstracts

ISBN

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ISSN

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e-ISSN

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Number of pages

1

Pages from-to

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Publisher name

ČVUT

Place of publication

Praha

Event location

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Event date

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Type of event by nationality

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UT code for WoS article

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