Aircraft Drag Reduction with Flexible Composite Surface Boundary Layer Control
- 著者名:
- Sinha, S. ( Oxford, MS )
- 掲載資料名:
- AIAA meeting papers on disc
- シリーズ名:
- AIAA Paper : AIAA Flow Control Conference
- シリーズ巻号:
- 2nd
- 発行年:
- 2004
- 通号:
- 2004-2121
- ペーパー番号:
- AIAA-2004-2121
- 出版情報:
- [Reston, Va.]: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- 言語:
- 英語
- 請求記号:
- A07400/200409 [CD-ROM 2004 Disc 9]
- 資料種別:
- テクニカルペーパー
類似資料:
|
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
|
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
|
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
|
American Institute of Aeronautics and Astronautics |
10
テクニカルペーパー
AN INVESTIGATION OF THE FEASIBILITY OF ACTIVE BOUNDARY LAYER THICKENING FOR AIRCRAFT DRAG REDUCTION Final
National Aeronautics and Space Administration |
|
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |
|
"Society of Automotive Engineering, Inc." |
12
テクニカルペーパー
Controlling an unsteady separating boundary layer on a cylinder with an active compliant wall
American Institute of Aeronautics and Astronautics |