LOW SPPED TESTING OF A LAMINAR FLOW AIRFOIL IN AN ADAPTIVE WALL WIND TUNNEL
- 著者名:
- Khadjavi, F. ( The Aeronautical Reseach Institute of Sweden )
- 掲載資料名:
- NASA Technical Reports
- 発行年:
- 1989
- 通号:
- N90-23363
- ペーパー番号:
- N90-23363
- 開始ページ:
- 1
- 終了ページ:
- 97
- 総ページ数:
- 97
- 出版情報:
- National Aeronautics and Space Adminstration
- 言語:
- 英語
- 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 |
9
テクニカルペーパー
WIND TUNNEL RESULTS FOR A HIGH-SPEED, NATURAL LAMINAR-FLOW AIRFOIL DESIGNED FOR GENERAL AVIATION AIRCRAFT
National Aeronautics and Space Administration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
テクニカルペーパー
A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |