Application of a Weighted Average Surrogate Approach to Helicopter Rotor Blade Vibration Reduction

Application of a Weighted Average Surrogate Approach to Helicopter Rotor Blade Vibration Reduction

Author(s):

B. Glaz ( The University of Michigan, Ann Arbor, MI )
T. Goel ( The University of Florida, Gainesville, FL )
L. Liu ( The University of Michigan, Ann Arbor, MI )
P. Friedmann
R. Haftka ( The University of Florida, Gainesville, FL )

Publication title:

AIAA meeting papers on disc

Title of ser.:

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

Ser. no.:

2007

Pub. Year:

2007

No.:

2007-1898

Paper no.:

AIAA Paper 2007-1898

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200707 [CD-ROM 2007 Disc 7]

Type:

Technical Paper

Details

TDL ID:	ZA00049495
Series ID:	PA00000154
Conf. info. (Name):	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Conf. info. (Number):	48th
Conf. info. (Venue):	Honolulu, Hawaii
Conf. info. (Date):	2007.04.23-2007.04.26

Similar Items:

1 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	7 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
2 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	8 Technical Paper Performance Estimate and Simultaneous Application of Multiple Surrogates T. Goel, R. Haftka, N. Queipo, W. Shyy American Institute of Aeronautics and Astronautics
3 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	9 Technical Paper Helicopter Noise Reduction By Actively Controlled Flaps Patt, D., Liu, L., Friedmann, P. American Institute of Aeronautics and Astronautics
4 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	10 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
5 Technical Paper A Computational Study of Microflaps with Application to Vibration Reduction in Helicopter Rotors Liu, Li, Padthe, Ashwani K., Friedmann, Peretz P. American Institute of Aeronautics and Astronautics	11 Technical Paper Error Measures for Noise-Free Surrogate Approximations T. Goel, R. Haftka, W. Shyy American Institute of Aeronautics and Astronautics
6 Technical Paper The AVINOR Aeroelastic Simulation Code and Its Application to Reduced Vibration Composite Rotor Blade Design Glaz, Bryan, Friedmann, Peretz, Liu, Li, Kumar, Devesh, Cesnik, Carlos American Institute of Aeronautics and Astronautics	12 Technical Paper Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips Yuan, K. A., Friedmann, P. P. National Aeronautics and Space Adminstration

1

2

3

4

5

6

7

8

9

10

11

12