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A reduced model for prediction of thermal and rotational effects on turbine tip clearance

A reduced model for prediction of thermal and rotational effects on turbine tip clearance

By Javier A. Kypuros

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Publish Date

2003

Publisher

National Aeronautics and Space Administration, Glenn Research Center

Language

eng

Pages

-

1-2 of 2 Editions

A reduced model for prediction of thermal and rotational effects on turbine tip clearance

View A reduced model for prediction of thermal and rotational effects on turbine tip clearance
A reduced model for prediction of thermal and rotational effects on turbine tip clearance

Language: eng

Published In: 2003

Publisher: National Aeronautics and Space Administration, Glenn Research Center

A reduced model for prediction of thermal and rotational effects on turbine tip clearance

View A reduced model for prediction of thermal and rotational effects on turbine tip clearance
A reduced model for prediction of thermal and rotational effects on turbine tip clearance

Language: eng

Published In: 2003

Publisher: National Aeronautics and Space Administration, Glenn Research Center