Compressor blade forced response due to downstream vane-strut potential interaction

Compressor blade forced response due to downstream vane-strut potential interaction

Author(s):

Chiang, Hsiao-Wei D. ( GE Aircraft Engines )
Turner, Mark G.

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Ser. no.:

1993

Pub. Year:

1993

No.:

93-GT-287

Paper no.:

93-GT-287

Pub. info.:

New York, NY: The American Society of Mechanical Engineers

Language:

English

Call no.:

A11800

Type:

Technical Paper

Details

TDL ID:	ZA00002294
Series ID:	PA00000136
Conf. info. (Name):	International Gas Turbine and Aeroengine Congress and Exposition
Conf. info. (Number):	1993
Conf. info. (Venue):	Cincinnati, Ohio
Conf. info. (Date):	1993.05.24-1993.05.27
Note for article:	Presented at the International Gas Turbine and Aeroengine Congress and Exposition Cincinnati, Ohio - May 24-27, 1993 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, 1993

Similar Items:

1 Technical Paper Turbine and compressor wake modeling for blade forced response Izsak, Michael S., Chiang, Hsiao-Wei D. The American Society of Mechanical Engineers	7 Technical Paper The influence of wake-wake interactions on loss fluctuations of a downstream axial compressor blade row Walker, G. J., Hughes, J D, Kohler, I, Solomon, W J The American Society of Mechanical Engineers
2 Technical Paper Influence of vaned diffuser on dangerous blade vibration due to blade flow interactions in a centrifugal compressor Jin, D., Jiang, Z., Hasemann, H., Haupt, U., Rautenberg, M. The American Society of Mechanical Engineers	8 Technical Paper Prediction of Shrouded Turbomachinery Blade Forced Response by a Complex Mode Analysis. Chiang, H-W.D., Hsu, C-N. American Society of Mechanical Engineers
3 Technical Paper A cyclic symmetry analysis for turbomachine blade flutter Chiang, Hsiao-Wei D., Chung, Meng-Hsuan The American Society of Mechanical Engineers	9 Technical Paper A Model of Compressor Blade Row Interaction with Shock Induced Vortex Shedding M. Turner, S. Gorrell, D. Car American Institute of Aeronautics and Astronautics
4 Technical Paper Passive control of flow induced vibrations by splitter blades Chiang, Hsiao-Wei,Z139 D., Fleeter, Sanford The American Society of Mechanical Engineers	10 Technical Paper Pressure Disturbances on Compressor Vanes Forced By Vortex Shedding From Downstream Cylinders. Wade, P.C., King, P.I., Jumper, E.J. American Institute of Aeronautics and Astronautics
5 Technical Paper Multistage turbine simulations with vortex-blade interaction Turner, Mark G. The American Society of Mechanical Engineers	11 Technical Paper Rotor blade-to-blade wake variability and its effect on downstream vane response Sanders, A., Fleeter, S. American Institute of Aeronautics and Astronautics
6 Conference Proceedings Prediction of Shrouded Turbomachinery Blade Forced Response by a Complex Mode Analysis Hsiao-Wei D. Chiang, Chih-Neng Hsu American Society of Mechanical Engineers	12 Technical Paper Forced Response of Shrouded Bladed Disk Assemblies: A Jointed Experimental Numerical Approach. D'Ambrosio, F., Chatelet, E., Ravoux, J., Jacquet-Richardet, G. American Society of Mechanical Engineers

1

2

3

4

5

6

7

8

9

10

11

12