Study of boundary layer development in a two-stage low-pressure turbine

Study of boundary layer development in a two-stage low-pressure turbine

著者名:

Dorney, D.J. ( Virginia Commonwealth University )
Ashpis, D.E. ( NASA Lewis Research Center )
Halstead, D.E. ( GE Aircraft Engines )
Wisler, D.C. ( GE Aircraft Engines )

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

シリーズ巻号:

1999

発行年:

1999

通号:

99-0742

ペーパー番号:

99-0742

開始ページ:

1

終了ページ:

23

出版情報:

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

詳細

TDL書誌ID:	ZA00050873
シリーズID:	PA00000138
会議名:	Aerospace Sciences Meeting and Exhibit
回次:	37th
会議開催地:	Reno, NV
会議開催年:	1999.01.11-1999.01.14
論文注記:	37th AIAA Aerospace Sciences Meeting and Exhibit, January 11-14, 1999/Reno, NV

類似資料:

1 テクニカルペーパー Study of Boundary Layer Development in a Two-Stage Low-Pressure Turbine Dorney, D. J., Ashpis, D. E., Halstead, D. E., Wisler, D. C. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Boundary layer development in axial compressors and turbines part 4 of 4: Computations & Analyses Halstead, David E., Walker, Gregory J., Wisler, David C., Hodson, Howard P., Okiishi, Theodore H., Shin, Hyoun-Woo The American Society of Mechanical Engineers
2 テクニカルペーパー Study of low Reynolds number effects on the losses in low-pressure turbine blade rows Dorney, D.J., Ashpis, D.E. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Effect of Reynolds Number and Periodic Unseady Wake Flow Condition on Boundary Layer Development, Separation, and Re- Attachment Along the Suction Surface of a … Qzturk, B., Schobeiri, M.T., Ashpis, D.E. American Society of Mechanical Engineers
3 テクニカルペーパー Effects of Blade Count on Boundary Layer Development in a Low-Pressure Turbine Dorney, Daniel J., Flitan, Horia C., Ashpis, David E., Solomon, William J. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Computational Study of clocking an Embedded Stage in a 4-Stage Industrial Turbine. Dorney, D.J., Croft, R.R., Sondak, D.L., Stang, U.E., Twardocleb, C.Z. American Society of Mechanical Engineers
4 テクニカルペーパー Boundary layer development in axial compressors and turbines part 2 of 4: Compressors Halstead, David E., Walker, Gregory J., Wisler, David C., Hodson, Howard P., Okiishi, Theodore H., Shin, Hyoun-Woo The American Society of Mechanical Engineers	10 テクニカルペーパー Experimental and Numerical Investigation of Losses in Low-Pressure Turbine Blade Rows Dorney, Daniel J., Lake, James P., King, Paul I., Ashpis, David E. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Boundary layer development in axial compressors and turbines part 3 of 4: LP turbines Halstead, David E., Walker, Gregory J., Wisler, David C., Hodson, Howard P., Okiishi, Theodore H., Shin, Hyoun-Woo The American Society of Mechanical Engineers	11 テクニカルペーパー Intermittent Behavior of the Separated Boundary Layer Along the Suction Surface of a Low Pressure Turbine Blade Under Periodic Unsteady Flow Conditions. Ozturk, B., Schobeiri, M.T., Ashpis, D.E. American Society of Mechanical Engineers
6 テクニカルペーパー Boundary layer development in axial compressors and turbines part 1 of 4: Composite picture Halstead, David E., Walker, Gregory J., Wisler, David C., Hodson, Howard P., Okiishi, Theodore H., Shin, Hyoun-Woo The American Society of Mechanical Engineers	12 テクニカルペーパー Effects of Endwall Geometry and Stacking on Two-Stage Supersonic Turbine Performance. Dorney, D.J., Griffin, L.W., Huber, F.W., Sondak, D.L. American Institute of Aeronautics and Astronautics

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