Boundary layer development in axial compressors and turbines part 4 of 4: Computations & Analyses
- 著者名:
Halstead, David E. ( GE Aircraft Engines ) Walker, Gregory J. Wisler, David C. Hodson, Howard P. Okiishi, Theodore H. Shin, Hyoun-Woo - 掲載資料名:
- A.S.M.E. paper
- シリーズ名:
- ASME Technical Paper : GT
- シリーズ巻号:
- 1995
- 発行年:
- 1995
- 通号:
- 95-GT-464
- ペーパー番号:
- 95-GT-464
- 出版情報:
- New York: The American Society of Mechanical Engineers
- 言語:
- 英語
- 請求記号:
- A11800
- 資料種別:
- テクニカルペーパー
類似資料:
The American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
The American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
3
テクニカルペーパー
Boundary layer development in axial compressors and turbines part 1 of 4: Composite picture
The American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
National Aeronautics and Space Adminstration |
11
テクニカルペーパー
Effects of Shrouded Stator Cavity Flows on Multistage Axial Compressor Aerodynamic Performance
National Aeronautics and Space Adminstration |
The American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |