Helicopter Noise Reduction By Actively Controlled Flaps

Helicopter Noise Reduction By Actively Controlled Flaps

著者名:

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

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA/CEAS Aeroacoustics Conference

シリーズ巻号:

11th

発行年:

2005

通号:

2005-2904

ペーパー番号:

AIAA Paper 2005-2904

出版情報:

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

ISSN:

10877215

言語:

英語

請求記号:

A07400/200510 [CD-ROM 2005 Disc 10]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001625
シリーズID:	PA00000149
会議名:	AIAA/CEAS Aeroacoustics Conference ; AIAA Aeroacoustics Conference
回次:	11th ; 26th
会議開催地:	Monterey, California
会議開催年:	2005.05.23-2005.05.25

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1 テクニカルペーパー Simultaneous Vibration and Noise Reduction in Rotorcraft ・Practical Implementation Issues Liu, L., Friedmann, P., Patt, D. American Institute of Aeronautics and Astronautics	7 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
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6 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	12 テクニカルペーパー 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

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