Application of the Impulse Model Using Elliptical Wings for Calculations of Propeller Aerodynamic Characteristics
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F99%3A02012408" target="_blank" >RIV/68407700:21220/99:02012408 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Application of the Impulse Model Using Elliptical Wings for Calculations of Propeller Aerodynamic Characteristics
Original language description
An application of the impulse model using a system of elliptical vortex distributions in the wake behind the lift surface for the calculation of local and integral aerodynamic characteristics ofpropellers.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
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Result continuities
Project
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Continuities
Z - Vyzkumny zamer (s odkazem do CEZ)
Others
Publication year
1999
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Vedecko-technický rozvoj letectva a protivzdušnej obrany
ISBN
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ISSN
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e-ISSN
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Number of pages
6
Pages from-to
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Publisher name
Vojenský letecký technický a skúšobný ústav
Place of publication
Košice
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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