An evaluation of the tip clearance effects on turbine efficiency for space propulsion applications considering liquid rocket engine using turbopumps-Reference-Cited by-同舟云学术

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An evaluation of the tip clearance effects on turbine efficiency for space propulsion applications considering liquid rocket engine using turbopumps

Published:2017-11 Issue: Volume:70 Page:55-65
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Lindquist Whitacker Luiz Henrique,Tomita Jesuino Takachi^ORCID,Bringhenti Cleverson^ORCID

Funder

ITA

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. A Method of Performance Estimation of Axial-Flow Turbines;Ainley,1951

2. Improvements to the Ainley–Mathieson method of turbine performance prediction;Dunham;J. Eng. Power,1970

3. Mean line prediction method for axial flow turbine efficiency;Kacker;J. Eng. Power,1982

4. An improved incidence losses prediction method for turbine airfoils;Moustapha;J. Turbomach.,1990

5. Effect of Tip Clearance on Performance of Small Axial Hydraulic Turbine;Boynton,1976

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