On transonic flow models for optimized design and experiment

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F14%3A00227326" target="_blank" >RIV/68407700:21220/14:00227326 - isvavai.cz</a>

Result on the web

<a href="http://dx.doi.org/10.1051/epjconf/20146702111" target="_blank" >http://dx.doi.org/10.1051/epjconf/20146702111</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1051/epjconf/20146702111" target="_blank" >10.1051/epjconf/20146702111</a>

Result language

angličtina

Original language name

On transonic flow models for optimized design and experiment

Original language description

In the paper the near sonic flow theory for flows with small perturbations to sonic parallel flow is developed. This theory stands on the basis of potential flow of a compressible fluid and enables to receive an exact solution of the flow parameters pasttransonic cusped airfoils and their geometrical description. Generated airfoil shapes are tested using CFD ANSYS Fluent code to validate the results. Obtained numerical results from all-round commercial code show good accordance with the theory and confirm their value for future work in transonic design.

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

—

Project

—

Continuities

S - Specificky vyzkum na vysokych skolach

Publication year

2014

Confidentiality

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

Article name in the collection

EFM 2013; Experimental Fluid Mechanics 2013

ISBN

978-80-260-5375-0

ISSN

2101-6275

e-ISSN

—

Number of pages

4

Pages from-to

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Publisher name

Technical University of Liberec

Place of publication

Liberec

Event location

Kutná Hora

Event date

Nov 19, 2013

Type of event by nationality

EUR - Evropská akce

UT code for WoS article

000343672100114