Investigation of confluent boundary layers in high-lift flows

Investigation of confluent boundary layers in high-lift flows

著者名:

Ying, S.X. ( The Boeing Company )
Spaid, F.W. ( The Boeing Company )
McGinley, C.B. ( NASA Langley Research Center )
Rumsey, C.L. ( NASA Langley Research Center )

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : AIAA Applied Aerodynamics Conference

シリーズ巻号:

1998

発行年:

1998

通号:

98-2622

ペーパー番号:

98-2622

開始ページ:

1

終了ページ:

16

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:	ZA00050851
シリーズID:	PA00000157
会議名:	AIAA Applied Aerodynamics Conference
回次:	16th
会議開催地:	Albuquerque, NM
会議開催年:	1998.06.15-1998.06.18
論文注記:	16th AIAA Applied Aerodynamics Conference, June 15-18, 1998/Albuquerque, New Mexico

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1 テクニカルペーパー Experimental investigation of the confluent boundary layer of a high-lift system Thomas, F.O., Liu, X., Nelson, R.C. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Experimental Results for a Hypersonic Nozzle/Afterbody Flow Field Spaid, Frank W., Hui, Frank C.L. National Aeronautics and Space Adminstration
2 テクニカルペーパー An Experimental Investigation of the Confluent Boundary Layer on a High-Lift System Thomas, F. O., Nelson, R. C. National Aeronautics and Space Adminstration	8 テクニカルペーパー Three- Dimensional Effects on Multi- Element High Lift Computations Rumsey, C.L., Lee- Rausch, E.M., Watson, R.D. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー High lift research program for a fighter-type, multi-element airfoil at high Reynolds numbers Hobbs, C.R., Spaid, F.W., Ely, W.L., Goodman, Wesley L. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Compressible Linear Stability of Confluent Wake/Boundary Layers Liou, W.W., Liu, F. American Institute of Aeronautics and Astronautics
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5 テクニカルペーパー Numerical Simulation of Confluent Wake/Boundary Layer Flows. Liu, F., Liou, W.W., Joslin, R.D. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Experimental Investigation of Turbulent Boundary Layer Relaminarization with Application to High-Lift Systems: Prelimanary Results Bourassa,C., Thomas,F., Nelson,R. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー 3-D High-Lift Flow-Physics Experiment ・Transition Measurements McGinley, C., Jenkins, L., Watson, R., Bertelrud, A. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Review of Orbiter Flight Boundary Layer Transition Data C. McGinley, S. Berry, G. Kinder, M. Barnwell, K. Wang, B. Kirk American Institute of Aeronautics and Astronautics

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