Endwall effects at two tip clearances in a multistage axial flow compressor with controlled diffusion blading

Endwall effects at two tip clearances in a multistage axial flow compressor with controlled diffusion blading

Author(s):

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Ser. no.:

1993

Pub. Year:

1993

No.:

93-GT-299

Paper no.:

93-GT-299

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 Leakage effects in the rotor tip-clearance region of a multistage axial compressor, Part 1: Innovative experiments. Ivey, P. C., Swoboda, M. The American Society of Mechanical Engineers	7 Technical Paper Measurement of tip-clearance flow in a multi-stage, axial flow compressor Foley, Andrew C., Ivey, Paul C. The American Society of Mechanical Engineers
2 Technical Paper Controlled-endwall-flow blading for multistage axial compressor rotor Inoue, M., Kuroumaru, M., Furukawa, M., Kinoue, Y., Tanino, T., Maeda, S., Okuno, K. The American Society of Mechanical Engineers	8 Technical Paper The Use of Commercially Available Capacitance Tip Clearance Probes for Tip-Timing of Aero-Engine Compressor Blades. Lawson, C., Ivey, P. American Institute of Aeronautics and Astronautics
3 Technical Paper Control of Tip Clearance Flows in Axial Compressors Bae, J., Breuer, K.S., Tan, C.S. American Institute of Aeronautics and Astronautics	9 Technical Paper A New Design for Tip Injection in Transonic Axial Compressors. Beheshti, B.H., Ghorbanian, K., Farhanieh, B., Teixeira, J.A., Ivey, P.C. American Society of Mechanical Engineers
4 Technical Paper Stator averaged, rotor blade-to-blade near wall flow in a multistage axial compressor with tip clearance variation Moyle, I. N., Walker, G. J., Shreeve, R. P. The American Society of Mechanical Engineers	10 Technical Paper Leakage effects in the rotor tip-clearance region of a multistage axial compressor, Part 2: Numerical modelling Politis, E. S., Giannakoglou, K. C., Papailiou, K. D. The American Society of Mechanical Engineers
5 Technical Paper Compressor Blade tip Timing Using Capacitance Tip Clearance Probes. Lawson, C., Ivey, P. American Society of Mechanical Engineers	11 Technical Paper An experimental examination of cantilevered and shrouded stators in a multistage axial compressor Swoboda, M., Ivey, P. C., Wenger, U., Gummer, V. The American Society of Mechanical Engineers
6 Technical Paper Parametric Study of Tip Clearance - Casing Treatment on Performance and Stability of a Transonic Axial Compressor. Beheshti, B., Teixeira, J. A., Ivey, P. C., Ghorbanian, K., Farhanieh, B. American Society of Mechanical Engineers	12 Technical Paper Casing Treatment and Blade Tip Configuration Effects on Controlled Gas Turbine Blade Tip/Shroud Rubs at Engine Conditions. Padova, C., Dunn, M.G., Barton, J., Turner, K., Turner, A. American Society of Mechanical Engineers

1

2

3

4

5

6

7

8

9

10

11

12