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Measurement of Unsteady Blade Surface Pressure on a Single Rotation Large Scale Advanced Prop-Fan With Angular and Wake Inflow at Mach Numbers From 0.02 to 0.70

Author(s):
Publication title:
NASA Technical Reports
Pub. Year:
1988
Issue:
NASA-CR-182123
No.:
G3/07 0310411
Pt.:
NAS 1.26:182123
Paper no.:
N91-10065
Page(from):
1
Page(to):
45
Pages:
45
Pub. info.:
National Aeronautics and Space Adminstration
Language:
English
Type:
Technical Paper

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