Heat transfer in high-pressure compressor gas turbine internal air systems: A rotating disc-cone cavity with axial throughflow

A Alexiou; NJ Hills; CA Long; AB Turner

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Heat transfer in high-pressure compressor gas turbine internal air systems: A rotating disc-cone cavity with axial throughflow

Journal article

Peer reviewed

Heat transfer in high-pressure compressor gas turbine internal air systems: A rotating disc-cone cavity with axial throughflow

A Alexiou, NJ Hills, CA Long and AB Turner

EXPERIMENTAL HEAT TRANSFER, Vol.13(4), pp.299-328

01/10/2000

Abstract

Science & Technology

Physical Sciences

Technology

Thermodynamics

Engineering

Mechanical

Engineering

ENGINEERING

MECHANICAL

THERMODYNAMICS

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Title: Heat transfer in high-pressure compressor gas turbine internal air systems: A rotating disc-cone cavity with axial throughflow
Creators: A Alexiou
NJ Hills
CA Long
AB Turner
Publication Details: EXPERIMENTAL HEAT TRANSFER, Vol.13(4), pp.299-328
Publisher: TAYLOR & FRANCIS INC
Date published: 01/10/2000
Date submitted: 17/05/2017
Identifiers: 99516683902346
Academic Unit: University of Surrey
Language: English
Resource Type: Journal article

Heat transfer in high-pressure compressor gas turbine internal air systems: A rotating disc-cone cavity with axial throughflow

Abstract

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