Perfomance of a High-Work, Low-Aspect-Ratio Turbine Stator Tested With a Realistic Inlet Radial Temperature Gradient

Perfomance of a High-Work, Low-Aspect-Ratio Turbine Stator Tested With a Realistic Inlet Radial Temperature Gradient

Author(s):

Stabe, Roy G. ( Lewis Research Center )
Schwab, John R.

Publication title:

NASA Technical Reports

Pub. Year:

1991

Issue:

NASA-TM-103738

No.:

G3/07 0007297

Pt.:

NAS 1.15:103738

Paper no.:

N91-20126

Page(from):

1

Page(to):

31

Pages:

31

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:

ZA00001427

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