Aerodynamic Data for Tip Section of Rotor with 52 Titanium Blades 1375 mm Long

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61388998%3A_____%2F14%3A00432289" target="_blank" >RIV/61388998:_____/14:00432289 - 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

Aerodynamic Data for Tip Section of Rotor with 52 Titanium Blades 1375 mm Long

Original language description

The paper deals with aerodynamic experimental investigation of prismatic blade cascade,that represents the tip section of the rotor comprising of 52 titanium blades 1375mm long. This rotor is designed for the last stage of low pressure cylinder of a large output steam turbine. Investigated tip section is characterised by supersonic inlet, large stagger angle and supersonic outlet. Selected data from optical and pneumatic measurements are presented.

Czech name

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Czech description

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Type

D - Article in proceedings

CEP classification

BK - Liquid mechanics

OECD FORD branch

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Project

<a href="/en/project/TA03020277" target="_blank" >TA03020277: Aerodynamics of Highly Loaded Blade Cascades</a><br>

Continuities

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year

2014

Confidentiality

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

Article name in the collection

Turbostroje 2014 - Sborník referátů

ISBN

978-80-260-6447-3

ISSN

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e-ISSN

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Number of pages

8

Pages from-to

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Publisher name

ZČU Plzeň

Place of publication

Plzeň

Event location

Plzeň

Event date

Sep 24, 2014

Type of event by nationality

CST - Celostátní akce

UT code for WoS article

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