Improved blade profile loss and deviation angle models for advanced transonic compressor bladings: Part II - A model for supersonic flow

Improved blade profile loss and deviation angle models for advanced transonic compressor bladings: Part II - A model for supersonic flow

Author(s):

Konig, W. M. ( Technical University of Darmstadt )
Hennecke, D. K.
Fottner, L.

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Pub. Year:

1994

No.:

94-GT-336

Paper no.:

94-GT-336

Pub. info.:

New York: The American Society of Mechanical Engineers

Language:

English

Call no.:

A11800

Type:

Technical Paper

Details

TDL ID:	ZA00005619
Series ID:	PA00000136
Note for article:	Presented at the International Gas Turbine and Aeroengine Congress and Exposition The Hague, Netherlands - June 13-16, 1994 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, 1994

Similar Items:

1 Technical Paper Improved blade profile loss and deviation angle models for advanced transonic compressor bladings: Part I - A model for subsonic flow Konig, W. M., Hennecke, D. K., Fottner, L. The American Society of Mechanical Engineers	7 Technical Paper Improved Profile Loss and Deviation Correlations for Axial- Turbine Blade Rows. Zhu, J., Sjolander, S.A. American Society of Mechanical Engineers
2 Technical Paper Automised Calibration of Empirical Loss-And Deviation Models for Compressor Blade Rows. Hansen, A., Kappis, W. American Society of Mechanical Engineers	8 Technical Paper Unsteady flow and whirl-inducing forces in axial-flow compressors. part II-analysis Ehrich, F. F., Spakovszky, Z. S., Martinez-Sanchez, M., Song, S. J., Wisler, D. C., Storace, A. F., Shin, H.-W., … American Society of Mechanical Engineers
3 Technical Paper SECONDARY FLOW SPANWISE DEVIATION MODEL FOR THE STATORS OF NASA MIDDLE COMPRESSOR STAGES Roberts, W. B., Sandercock, D. M. National Aeronautics and Space Administration	9 Technical Paper Vortical Flow Structure and Loss Generation Process in Transonic Centrifugal Compressor Impeller. Ibaraki, S., Furukawa, M., Iwakiri, K., Takahashi, K. American Society of Mechanical Engineers
4 Technical Paper Turbine Blade Entropy generation rate part II: The measured loss O'Donnell, F. K., Davies, M. R. D. American Society of Mechanical Engineers	10 Technical Paper Numerical investigation of the flow in an aft-swept transonic compressor rotor Blaha, Christoph, Kablitz, Stephan, Hennecke, Dietmar K., Schmidt-Eisenlohr, Uwe, Pirker, Klaus, Haselhoff, Susanne American Society of Mechanical Engineers
5 Technical Paper Analysis and prediction of transonic turbine blade losses Farn, C. L. S., Whirlow, D. K., Chen, S. The American Society of Mechanical Engineers	11 Technical Paper Periodical Unsteady Flow within a Rotor Blade Row of an Axial Compressor: Part II - Wake-Tip Clearance Vortex Interaction. Mailach, R., Lehmann, I., Vogeler, K. American Society of Mechanical Engineers
6 Technical Paper Blade vibrations of a high speed compressor blisk-rotor - numerical resonance tuning and optical measurements - Frischbier, J., Schulze, G., Zielinski, M., Ziller, G., Blaha, C., Hennecke, D. K. The American Society of Mechanical Engineers	12 Technical Paper Viscous flow field computations for a transonic axial-flow compressor blade using different turbulence models Lenke, L. J., Simon, H. The American Society of Mechanical Engineers

1

2

3

4

5

6

7

8

9

10

11

12