Flow Field in the Compressor Blade Cascade NACA 65-100

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F10%3A00176539" target="_blank" >RIV/68407700:21220/10:00176539 - isvavai.cz</a>

Result on the web

—

DOI - Digital Object Identifier

—

Result language

angličtina

Original language name

Flow Field in the Compressor Blade Cascade NACA 65-100

Original language description

An investigation is made into the effects of a flow field in the compressor blade cascade NACA 65-100. This task has two main sections to explore, the transonic flows and the transition model. The transition model is consists of the laminar flow and theturbulent flow. These sections are solving via the CFD software ANSYS Fluent.

Czech name

—

Czech description

—

Type

D - Article in proceedings

CEP classification

BK - Liquid mechanics

OECD FORD branch

—

Project

<a href="/en/project/GA101%2F08%2F1112" target="_blank" >GA101/08/1112: Boundary layers separation control</a><br>

Continuities

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year

2010

Confidentiality

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

Article name in the collection

Fluid Mechanics and Thermodynamics

ISBN

80-86786-31-5

ISSN

—

e-ISSN

—

Number of pages

16

Pages from-to

—

Publisher name

Gradient

Place of publication

Praha

Event location

Praha

Event date

Mar 30, 2010

Type of event by nationality

EUR - Evropská akce

UT code for WoS article

—