Structural Tailoring of Aircraft Engine Blade Subject to Ice Impact Constraints

Structural Tailoring of Aircraft Engine Blade Subject to Ice Impact Constraints

Author(s):

Reddy, E.S. ( National Aeronautics and Space Administration Lewis Research Center )
Abumeri, G.H.
Murthy, P.L.N.
Chamis, C.C.

Publication title:

NASA Technical Reports

Pub. Year:

1993

Issue:

NASA-TM-106033

Pt.:

NAS 1.15:106033

Paper no.:

N93-26999

Page(from):

1

Page(to):

22

Pages:

22

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:

ZA00001429

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