Analysis and testing of Mach scaled rotor model with piezoelectric bender actuated trailing-edge flaps for helicopter vibration control

Analysis and testing of Mach scaled rotor model with piezoelectric bender actuated trailing-edge flaps for helicopter vibration control

Author(s):

Koratkar, Nikhil A. ( University of Maryland )
Chopra, Inderjit

Publication title:

A collection of technical papers : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, St. Louis MO, 12-15 April 1999

Title of ser.:

AIAA Paper : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Ser. no.:

1999

Pub. Year:

1999

Vol.:

pt. 4

No.:

99-1501

Paper no.:

AIAA 99-1501

Page(from):

2380

Page(to):

2402

Pub. info.:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563472930 [1563472937]

Language:

English

Call no.:

A07400/991201

Type:

Technical Paper

Details

TDL ID:	ZA00003932
Series ID:	PA00000154
Conf. info. (Name):	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit
Conf. info. (Venue):	St. Louis, MO
Conf. info. (Date):	1999.04.12-1999.04.15

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