Simultaneous Vibration and Noise Reduction in Rotorcraft ・Practical Implementation Issues

Simultaneous Vibration and Noise Reduction in Rotorcraft ・Practical Implementation Issues

著者名:

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

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

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

シリーズ巻号:

46th

発行年:

2005

通号:

2005-2245

ペーパー番号:

AIAA Paper 2005-2245

出版情報:

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

ISSN:

10877215

言語:

英語

請求記号:

A07400/200507 [CD-ROM 2005 Disc 7

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001622
シリーズID:	PA00000154
会議名:	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
回次:	46th
会議開催地:	Austin, Texas
会議開催年:	2005.04.18-2005.04.21

類似資料:

1 テクニカルペーパー Rotorcraft Vibration and Noise Prediction Using a Unified Aeroelastic Analysis Friedmann, P., Liu, L., Patt, D. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー 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
2 テクニカルペーパー Helicopter Noise Reduction By Actively Controlled Flaps Patt, D., Liu, L., Friedmann, P. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー 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
3 テクニカルペーパー The HHC Algorithm for Helicopter Vibration Reduction Revisited Patt, D., Liu, L., Chandrasekar, J., Bernstein, D., Friedmann, P. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー 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
4 テクニカルペーパー 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	10 テクニカルペーパー Actuator Saturation and its Influence on Vibration Reduction by Actively Controlled Flaps Cribbs,R., Friedmann,P. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー 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	11 テクニカルペーパー Reduction of Vibrations due to Dynamic Stall in Helicopters using an Actively Controlled Flap Friedmann, P., Depailler, G. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー 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	12 テクニカルペーパー 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

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