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Reduction of helicopter blade vortex interaction noise by active rotor control technology.
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Search Results - Reduction of helicopter blade vortex interaction noise by active rotor control technology.
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Active control
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Aircraft noise
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Control systems design
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Harmonic control
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Reduction of helicopter blade vortex interaction noise by active rotor control technology.
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Reduction
of
helicopter
blade
-
vortex
interaction
noise
by active rotor control technology
Published 1997
“…
Reduction
of
helicopter
blade
vortex
interaction
noise
…”
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Microfilm
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Format
Book
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Government Document
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Microfilm
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Norlin
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United States. National Aeronautics and Space Administration
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Yu, Yung H.
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English
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NASA technical memorandum
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NASA/TM
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