Investigation and Improvement of High-Lift Aerodynamic Performances in Lowspeed Wind Tunnel Testing

Investigation and Improvement of High-Lift Aerodynamic Performances in Lowspeed Wind Tunnel Testing

著者名:

Y. Yokokawa ( Japan Aerospace Exploration Agency, Chofu, Tokyo, Japan )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

シリーズ巻号:

2008

発行年:

2008

通号:

2008-0350

ペーパー番号:

AIAA Paper 2008-0350

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200801 [CD-ROM 2008 Disc 1]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00049519
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	46th
会議開催地:	Reno, Nevada
会議開催年:	2008.01.07-2008.01.10
論文注記:	46th AIAA Aerospace Sciences Meeting and Exhibit, 7-10 January 2008, Reno, Nevada

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1 テクニカルペーパー Numerical Simulation of Half-Span Aircraft Model with High-Lift Devices in Wind Tunnel M. Murayama, Y. Yokokawa, K. Tanaka, K. Yamamoto, T. Ito American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Investigation of Airframe Noise from High Lift Configuration Model H. Ura, Y. Yokokawa, T. Imamura, T. Ito, K. Yamamoto American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Efficient Design Exploration of Nacelle Chine Installation in Wind Tunnel Testing M. Kanazaki, Y. Yokokawa, M. Murayama, T. Ito, S. Jeong American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Phased Array Measurement of High Lift Devices in Low Speed Wind Tunnel H. Ura, Y. Yokokawa, T. Ito American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Experiment and CFD of a High-Lift Configuration Civil Transport Aircraft Model Y. Yokokawa, M. Murayama, T. Ito, K. Yamamoto American Institute of Aeronautics and Astronautics	9 テクニカルペーパー CFD Validation Study for a High-Lift Configuration of a Civil Aircraft Model M. Murayama, Y. Yokokawa, K. Yamamoto, Y. Ueda American Institute of Aeronautics and Astronautics
4 テクニカルペーパー PIV Investigation of Nacelle Chine Effects on High-Lift System Performance H. Kato, S. Watanabe, M. Murayama, Y. Yokokawa, T. Ito American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Multi-Objective Aerodynamic Optimization of Elements' Setting for High-lift Airfoil Using Kriging Model M. Kanazaki, K. Tanaka, S. Jeong, K. Yamamoto American Institute of Aeronautics and Astronautics
5 テクニカルペーパー High-Lift Device Testing in JAXA 6.5M X 5.5M Low-Speed Wind Tunnel T. Ito, Y. Yokokawa, H. Ura, H. Kato, K. Mitsuo, K. Yamamoto American Institute of Aeronautics and Astronautics	11 テクニカルペーパー High-Lift Wing Design in Consideration of Sweep Angle Effect Using Kriging Model M. Kanazaki, T. Imamura, S. Jeong, K. Yamamoto American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Studies on Airframe Noise Generation at High-lift Devices in Relation to Aerodynamic Performances Y. Yokokawa, T. Imamura, H. Ura, H. Uchida, T. Ito,, K. Yamamoto American Institute of Aeronautics and Astronautics	12 テクニカルペーパー PIV Measurement of a High-Lift-Device Model in JAXA 6.5m ﾗ 5.5m Low-Speed Wind Tunnel H. Kato, S. Watanabe, T. Hashimoto, K. Fujii, T. Ito, K. Yamamoto American Institute of Aeronautics and Astronautics

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