The Wing Lift Distribution Formed by a Variable Free Stream Velocity Vectors in Airplane Flow Fields
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F99%3A02012398" target="_blank" >RIV/68407700:21220/99:02012398 - 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
The Wing Lift Distribution Formed by a Variable Free Stream Velocity Vectors in Airplane Flow Fields
Original language description
Using of the impulse model formed by a system of elementary wings for the determination of the lift wing distribution under a non-unifor free flow.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
BK - Liquid mechanics
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
Fluid Mechanics and Thermodynamics
ISBN
80-902714-1-3
ISSN
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e-ISSN
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Number of pages
4
Pages from-to
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Publisher name
Gradient
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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