Reduction of helicopter blade-vortex interaction noise by active rotor control technology [microform] / Yung H. Yu [and others]

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Bibliographic Details
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Yu, Yung H.
Other title:	Reduction of helicopter blade vortex interaction noise by active rotor control technology.
Format:	Government Document Microfilm Book
Language:	English
Published:	[Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], [1997]
Series:	NASA technical memorandum ; 207568.
Subjects:	Active control. Blade-vortex interaction. Control systems design. Smart structures. Structural design. Helicopters. Aircraft noise. Harmonic control.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:207568
NAS 1.15:207568	Restricted Place a Hold