Effect of reduced aft diameter and increased blade number on high-speed counterrotation propeller performance

Effect of reduced aft diameter and increased blade number on high-speed counterrotation propeller performance

Author(s):

Rose, Gayle E. ( Sverdrup Technology )
Jeracki, Robert J. ( NASA Lewis Research Center )

Publication title:

NASA Technical Reports

Pub. Year:

1989

Issue:

NASA-TM-102077

No.:

G3/02 0252510

Pt.:

NAS 1.15:102077

Paper no.:

N90-13352

Page(from):

1

Page(to):

31

Pages:

31

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:

ZA00001426

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