A Non-Intrusive Sensing Technique to Infer Optimal Flow Control in Serpentine Inlets

A Non-Intrusive Sensing Technique to Infer Optimal Flow Control in Serpentine Inlets

著者名:

J. Anderson ( Techsburg, Inc., Blacksburg, VA )

W. Ng ( Virginia Polytechnic Institute and State University, Blacksburg, VA )

R. Burdisso

P. Truax ( Lockheed Martin Aeronautics Company, Fort Worth, TX )

D. Miller

M. Niestroy

さらに 1 件

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:

2006

発行年:

2006

通号:

2006-0013

ペーパー番号:

AIAA Paper 2006-13

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200601 [CD-ROM 2006 Disc 1]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00047216
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	44th
会議開催地:	Reno, Nevada
会議開催年:	2006.01.09-2009.01.12

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1 テクニカルペーパー A Facility for Active Flow Control Research in Serpentine Inlets. Rabe, A., Olcmen, S., Anderson, J., Burdisso, R., Ng, W. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Sensing for Active Flow Control in Advanced Propulsion-Airframe Integration Systems Fleming, J., Olcman, S., Burdisso, R., Ng, W. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Effectiveness of a Serpentine Inlet Duct Flow Control Technique at Design and Off-Design Simulated Flight Conditions. Rabe, A., Ng, W., Burdisso, R. American Society of Mechanical Engineers	8 テクニカルペーパー Fan Flow Control for Noise Reduction Part 3: Rig Testing of Optimal Design Langford, M., Minton, C., Ng, W., Burdisso, R., Halasz, C. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Boundary Layer Control and Wall-Pressure Fluctuations in a Serpentine Inlet Harper, D. K., Leitch, T. A., Ng, W. F., Guillot, S. G., Burdisso, R. A. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Fan Flow Control for Noise Reduction Part 1: Advanced Trailing Edge Blowing Concepts Halasz, C., Arntz, D., Burdisso, R., Ng, W. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー A Technique to Estimate Flow Distortion in Boundary Layer Ingesting Serpentine Inlets Using Unsteady Wall-Pressures J. Anderson, W. Ng, J. Fleming American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Screening of Potential Noise Control Devices at Virginia Tech for QTD II Flight Test P. Ravetta, R. Burdisso, W. Ng, M. Khorrami, R. Stoker American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Fan Flow Control for Noise Reduction Part 2: Investigation of Wake-Filling Techniques Langford, M., Minton, C., Ng, W., Estevadeordal, J., Burdisso, R. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Noise Control of Landing Gears Using Elastic Membrane-Based Fairings P. Ravetta, R. Burdisso, W. Ng American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Experimental Investigation of Active Flow Control of a Boundary Layer Ingesting Serpentine Inlet Diffuser N. Harrison, J. Anderson, J. Fleming, W. Ng American Institute of Aeronautics and Astronautics	12 テクニカルペーパー AFT Fan Noise Control Using Herschel/Quincke-Liner Systems De La Riva, D., Burdisso, R., Ng, W. American Institute of Aeronautics and Astronautics

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