Density and Mach Number Effects on Piezoelectric Flow Control Actuator Performance
- 著者名:
- Chambers,F.W. ( Oklahoma State University )
- Jones,G.S. ( NASA Langley Research Center )
- 掲載資料名:
- AIAA paper
- シリーズ名:
- AIAA Paper : AIAA Fluid Dynamics Conference
- シリーズ巻号:
- 2001
- 発行年:
- 2001
- 通号:
- 2001-3025
- ペーパー番号:
- AIAA-2001-3025
- 開始ページ:
- 1
- 終了ページ:
- 15
- 総ページ数:
- 15
- 出版情報:
- Reston, VA: American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- 言語:
- 英語
- 請求記号:
- A07400
- 資料種別:
- テクニカルペーパー
類似資料:
American Institute of Aeronautics and Astronautics |
7
テクニカルペーパー
Piezoelectric actuator-active vibration control of the shaft line for a gas turbine engine test stand
The American Society of Mechanical Engineers |
Society of Automotive Engineering, Inc. |
Society of Automotive Engineering, Inc. |
Society of Automotive Engineers |
9
テクニカルペーパー
Simulation of the Effects of Force and Heat Produced by a Plasma Actuator on Neutral Flow Evolution
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
Society of Automotive Engineers |
The American Society of Mechanical Engineers |
National Aeronautics and Space Adminstration |
6
テクニカルペーパー
An Active Flow Circulation Controlled Flap Concept for General Aviation Aircraft Applications.
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |