Numerical Data Analysis of Transonic Flow Past Cusped Airfoil
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F14%3A00222835" target="_blank" >RIV/68407700:21220/14:00222835 - 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
Numerical Data Analysis of Transonic Flow Past Cusped Airfoil
Original language description
Transonic flow past two cusped airfoils is numerically solved and achieved results are analyzed by means of fow behavior and oblique shocks formation. Regions around sharp trailing edges are studied in detail and parameters of shock waves are solved andcompared using classical shock polar approach and verified by reduction parameters for symmetric configurations.
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
S - Specificky vyzkum na vysokych skolach
Others
Publication year
2014
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
33. Setkání kateder mechaniky tekutin a termomechaniky
ISBN
978-80-01-05538-0
ISSN
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e-ISSN
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Number of pages
4
Pages from-to
88-91
Publisher name
ČVUT
Place of publication
Praha
Event location
Praha
Event date
Sep 9, 2014
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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