EXPERIMENTAL RESULTS FOR A TWO-DIMENSIONAL SUPERSONIC INLET USED AS A THRUST DEFLECTING NOZZLE
- 著者名:
- Johns, Albert L. et al. ( NASA )
- 掲載資料名:
- NASA Technical Reports(N89)
- 発行年:
- 1984
- 号:
- NASA-TM-83439
- 通号:
- G3/34 0164878
- パート:
- NAS1.15:83439
- ペーパー番号:
- N89-14386
- 開始ページ:
- 1
- 終了ページ:
- 14
- 総ページ数:
- 14
- 出版情報:
- National Aeronautics and Space Administration
- 言語:
- 英語
- 資料種別:
- テクニカルペーパー
類似資料:
National Aeronautics and Space Adminstration |
National Aeronautics and Space Adminstration |
2
テクニカルペーパー
Experimental and numerical study of the fluidic thrust vectoring of a two-dimensional supersonic nozzle
American Institute of Aeronautics and Astronautics |
8
テクニカルペーパー
Engine Inlet Distortion in a 9.2 Percent Scale Vectored Thrust STOVL Model in Groud Effect
National Aeronautics and Space Adminstration |
3
テクニカルペーパー
Flow Visualization and Interpretation of Visualization Data for Deflected Thrust V/STOL Nozzles
National Aeronautics and Space Administration |
National Aeronautics and Space Adminstration |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
11
テクニカルペーパー
An experimental Investigation of Two-Dimensional Thrust Augmenting Ejectors: Final Report, Part 2
National Aeronautics and Space Administration |
National Aeronautics and Space Adminstration |
12
テクニカルペーパー
An Experimental Investigation of Two-Dimensional Thrust Augmenting Ejectors: Final Report, Part 1
National Aeronautics and Space Administration |