Helicopter Noise Reduction By Actively Controlled Flaps

Helicopter Noise Reduction By Actively Controlled Flaps

Author(s):

Patt, D. ( University of Michigan, Ann Arbor, MI )
Liu, L.
Friedmann, P.

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA/CEAS Aeroacoustics Conference

Ser. no.:

11th

Pub. Year:

2005

No.:

2005-2904

Paper no.:

AIAA Paper 2005-2904

Pub. info.:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200510 [CD-ROM 2005 Disc 10]

Type:

Technical Paper

Details

TDL ID:	ZA00001625
Series ID:	PA00000149
Conf. info. (Name):	AIAA/CEAS Aeroacoustics Conference ; AIAA Aeroacoustics Conference
Conf. info. (Number):	11th ; 26th
Conf. info. (Venue):	Monterey, California
Conf. info. (Date):	2005.05.23-2005.05.25

Similar Items:

1 Technical Paper Simultaneous Vibration and Noise Reduction in Rotorcraft ・Practical Implementation Issues Liu, L., Friedmann, P., Patt, D. American Institute of Aeronautics and Astronautics	7 Technical Paper Vibration Reduction and Performance Enhancement of Helicopter Rotors Using an Active/Passive Approach B. Glaz, P. Friedmann, L. Liu American Institute of Aeronautics and Astronautics
2 Technical Paper The HHC Algorithm for Helicopter Vibration Reduction Revisited Patt, D., Liu, L., Chandrasekar, J., Bernstein, D., Friedmann, P. American Institute of Aeronautics and Astronautics	8 Technical Paper Actuator Saturation and its Influence on Vibration Reduction by Actively Controlled Flaps Cribbs,R., Friedmann,P. American Institute of Aeronautics and Astronautics
3 Technical Paper Reduction of Vibrations due to Dynamic Stall in Helicopters using an Actively Controlled Flap Friedmann, P., Depailler, G. American Institute of Aeronautics and Astronautics	9 Technical Paper Surrogate Based Optimization of Helicopter Rotor Blades for Vibration Reduction in Forward Flight B. Glaz, P. Friedmann, L. Liu American Institute of Aeronautics and Astronautics
4 Technical Paper Rotorcraft Vibration and Noise Prediction Using a Unified Aeroelastic Analysis Friedmann, P., Liu, L., Patt, D. American Institute of Aeronautics and Astronautics	10 Technical Paper Efficient Global Optimization of Helicopter Rotor Blades for Vibration Reduction in Forward Flight B. Glaz, P. Friedmann, L. Liu American Institute of Aeronautics and Astronautics
5 Technical Paper Vibration Reduction and Performance Enhancement in Rotorcraft Using Active Flaps at High Advance Ratios L. Liu, P. Friedmann, I. Kim, D. Bernstein American Institute of Aeronautics and Astronautics	11 Technical Paper Application of a Weighted Average Surrogate Approach to Helicopter Rotor Blade Vibration Reduction B. Glaz, T. Goel, L. Liu, P. Friedmann, R. Haftka American Institute of Aeronautics and Astronautics
6 Technical Paper Vibration reduction in helicopter rotors using an actively controlled partial span trailing edge flap located on the blade Millott, T. A., Friedmann, P. P. National Aeronautics and Space Adminstration	12 Technical Paper Unsteady compressible aerodynamics of a flapped airfoil with application to helicopter vibration reduction Myrtle, Timothy F., Friedmann, Peretz P. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12