Design and Numerical Calculation of Variable Test Section for Small Supersonic Wind Tunnel

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F46747885%3A24210%2F10%3A%230001635" target="_blank" >RIV/46747885:24210/10:#0001635 - 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
Design and Numerical Calculation of Variable Test Section for Small Supersonic Wind Tunnel
Original language description
The article deals with design and numerical calculation of a variable test section for small supersonic wind tunnel. The supersonic wind tunnel is designed to be driven by a supersonic ejector. The test section, which is in focus, is considered to by placed on its suction inlet. Schlieren method will be used to investigate the flow within. The purpose of the test section is to demonstrate effects, which occur in supersonic flows, e.g. shock waves, interactions of shock waves with boundary layers etc.
Czech name
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Czech description
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Project
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Continuities
Z - Vyzkumny zamer (s odkazem do CEZ)<br>I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
XXIX. setkání kateder mechaniky tekutin a termomechaniky
ISBN
9788024822440
ISSN
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e-ISSN
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Number of pages
326
Pages from-to
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Publisher name
Vysoká škola báňská - TU Ostrava
Place of publication
Vysoká škola báňská - TU Ostrava
Event location
Rožnov pod Radhoštěm
Event date
Jan 1, 2010
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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