Unsteady pressures on a blunt trailing edge - end plate & boundary layer effects | 東京工業大学附属図書館文献データベース

Unsteady pressures on a blunt trailing edge - end plate & boundary layer effects

著者名:

Vassilopoulos, K. ( University College, U.N.S.W., Australian Defence Force Academy )
Gai, S.L. ( University College, U.N.S.W., Australian Defence Force Academy )

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:

1998

発行年:

1998

通号:

98-0418

ペーパー番号:

98-0418

開始ページ:

1

終了ページ:

10

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:	ZA00050859
シリーズID:	PA00000138
会議名:	Aerospace Sciences Meeting and Exhibit
回次:	36th
会議開催地:	Reno, NV
会議開催年:	1998.01.12-1998.01.15
論文注記:	36th Aerospace Sciences Meeting & Exhibit, January 12-15, 1998/Reno, NV

類似資料:

1 テクニカルペーパー Unsteady flow computations of a slat with a blunt trailing edge Khorrami, Mehdi R., Berkman, Mert E., Choudhari, Meelan, Singer, Bart A., Lockard, David P., Brentner, Kenneth S. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Numerical study of unsteady shock/boundary-layer interaction induced by a blunt fin Yamamoto, S., Takasu, N. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー EXPERIMENTAL ANALYSES OF TRAILING EDGE FLOWS Final Technical Report Petrie, S.L. National Aeronautics and Space Administration	8 テクニカルペーパー Predicting Modes of a Turbulent Boundary Layer for Trailing Edge Noise Calculations Spitz, N., Devenport, W., Glegg, S. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Effects of periodic unsteady wake flow and pressure gradient on boundary layer transition along the concave surface of a curved plate Schobeiri, M. T., Radke, R. E. The American Society of Mechanical Engineers	9 テクニカルペーパー Unsteady boundary layers on a flat plate disturbed by periodic wakes : Part II - Measurements of unsteady boundary layers and discussion Funazaki, K. The American Society of Mechanical Engineers
4 テクニカルペーパー Analysis of Blunt Trailing Edge Airfoils Standish, K., Dam, C. van American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Heat Transfer and Pressure Measurements in a Lattice-Cooled Trailing Edge of a Turbine Airfoil. Saha, K., Guo, S., Acharya, S., Nakamata, C. American Society of Mechanical Engineers
5 テクニカルペーパー Hypersonic boundary-layer stability over blunt leading edges with bow-shock effects Hu, Sean H., Zhong, Xiaolin American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Theoretical Analysis of Unswept Normal Shock Wave/Boundary Layer Interaction Control Using Streamwise Flaps J. Couldrick, S. Gai, J. Milthorpe, K. Shankar American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Effects of Nose Bluntness on Stability of Hypersonic Boundary Layers over a Blunt Cone K. Kara, P. Balakumar, O. Kandil American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Swept Shock Wave/ Turbulent Boundary Layer Interaction Control with ﾔSmart' Flap Actuators. Couldrick, J., Gai, S., Milthorpe, J., Shankar, K. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12