The effect of periodic ribs on the local aerodynamic and heat transfer performance of a straight cooling channel

The effect of periodic ribs on the local aerodynamic and heat transfer performance of a straight cooling channel

著者名:

Rau, G. ( von Karman Institute )
Moeller, D.
Cakan, M.
Arts, T.

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:

1996

発行年:

1996

通号:

96-GT-541

ペーパー番号:

96-GT-541

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

詳細

TDL書誌ID:	ZA00002367
シリーズID:	PA00000136
会議名:	International Gas Turbine and Aeroengine Congress & Exhibition
回次:	1996
会議開催地:	Birmingham, UK
会議開催年:	1996.06.10-1996.06.13
論文注記:	Presented at the International Gas Turbine and Aeroengine Congress & Exhibition Birmingham, UK - June 10-13, 1996 This paper has been accepted for publication in the Transactions of the ASME Discussion of it will be accepted at ASME Headquarters until September 30, 1996

類似資料:

1 テクニカルペーパー Conjugate Heat Transfer Investigation of Rib-Roughened Cooling Channels. Agostini, F., Arts, T. American Society of Mechanical Engineers	7 テクニカルペーパー Heat Transfer in Rotating Rectangular Cooling Channels with Angled Ribs Griffith,T.S., Al-Hadhrami,L., Han,J.C. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Aero-Thermal Investigation of a Rib-Roughened Trailing Edge Channel with Crossing-Jets. Part II: Heat Transfer Analysis. Coletti, F., Armellini, A., Arts, T., Schpltes, C. American Society of Mechanical Engineers	8 テクニカルペーパー Experimental heat transfer and friction in channels roughened with angled, V-shaped and discrete ribs on two opposite walls Taslim, M. E., Li, T., Kercher, D. M. The American Society of Mechanical Engineers
3 テクニカルペーパー Investigation of the Conjugate Convective-Conductive Thermal Behavior of a Rib-Roughened Internal Cooling Channel. Fedrizzi, R., Arts, T. American Society of Mechanical Engineers	9 テクニカルペーパー EFFECT of Rib Turbulators in The First Pass on Heat Transfer Distributions In a Two-Pass Channel Connected By Two Rows of Holes. Ekkad, S.V., Kontrovitz, D., Nasir, H., Pamula, G., Acharya, S. American Society of Mechanical Engineers
4 テクニカルペーパー Surface heating effect on local heat transfer in a rotating two-pass square channel with 60｡?angled rib turbulators Zhang, Y. M., Han, J. C., Parsons, J. A., Lee, C. P. The American Society of Mechanical Engineers	10 テクニカルペーパー Measurements of heat transfer coefficients and friction factors in rib-roughened channels simulating leading-edge cavities of a modern turbine blade Taslim, M.E., Li, T., Spring, S.D. The American Society of Mechanical Engineers
5 テクニカルペーパー The Effect of Ribs and Tip Wall Distance on Heat Transfer for a Varying Aspect Ratio Two-Pass Ribbed Internal Cooling Channel. Jenkins, S.C., Zehnder, F., Shevchuk, I.V., Weigand, B., Schnieder, M. American Society of Mechanical Engineers	11 テクニカルペーパー Local heat transfer and flow structure on and above a dimpled surface in a channel Mahmood, G. I., Hill, M. L., Nelson, D. L., Ligrani, P. M., Moon, H.-K., Glezer, B. American Society of Mechanical Engineers
6 テクニカルペーパー Heat Transfer in Leading Edge, Triangular Shaped Cooling Channels with Angled Ribs Under High Rotation Numbers. Liu, Y-H., Huh, M., Rhee, D-H., Han, J-C., Moon, H-K. American Society of Mechanical Engineers	12 テクニカルペーパー Experimental and analytical investigation of local heat transfer in high aspect ratio cooling channels Neuner, F., Preclik, D., Popp, M., Funke, M., Kluttig, H. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12