Unsteady Pressure Field Due to Interactions Among Tip Leakage Vortex, Trailing Edge Vortex, and Vortex Shedding in a Ducted Propeller

Unsteady Pressure Field Due to Interactions Among Tip Leakage Vortex, Trailing Edge Vortex, and Vortex Shedding in a Ducted Propeller

Author(s):

Publication title:

ASME Turbo Expo 2007: Power for Land, Sea, and Air (GT2007)

Title of ser.:

ASME Symposia Volumes

Ser. no.:

TURBO EXPO 2007(6B)

Pub. Year:

2007

Vol.:

6B

Paper no.:

GT2007-27407

Page(from):

1639

Page(to):

1646

Pages:

8

Pub. info.:

New York: American Society of Mechanical Engineers

ISBN:

9780791847954 [0791847950]

Language:

English

Call no.:

A11661/2007

Type:

Conference Proceedings

Details

TDL ID:	ZA00048744
Series ID:	PA00000270
Conf. info. (Name):	ASME Turbo Expo
Conf. info. (Number):	2007
Conf. info. (Venue):	Montreal, Canada
Conf. info. (Date):	2007.05.14-2007.05.17

Similar Items:

1 Technical Paper Unsteady Pressure Field Due to Interactions Among Tip Leakage Vortex, Trailing Edge Vortex, and Vortex Shedding in a Ducted Propeller. Hah, C., Lee, Y.-T. American Society of Mechanical Engineers	7 Technical Paper The Tip Leakage Vortex Shed from an Unsteady Tip Clearance Flow Intaratep, N., Devenport, W., Staubs, J. American Institute of Aeronautics and Astronautics
2 Conference Proceedings Tip Clearance Vortex Oscillation, Vortex Shedding and Rotating Instabilities in an Axial Transonic Compressor Rotor Chunill Hah, Jörg Bergner, Heinz-Peter Schiffer American Society of Mechanical Engineers	8 Technical Paper The effect of vortex shedding on the unsteady pressure distribution around the trailing edge of a turbine blade Cicatelli, G., Sieverding, C. H. The American Society of Mechanical Engineers
3 Technical Paper Numerical study of the tip clearance flow development in a propulsion pump stage Lee, Yu-Tai, Hah, Chunill, Loellbach, James The American Society of Mechanical Engineers	9 Conference Proceedings A Numerical Investigation of the Interaction Between Rotor Bow Waves and Upstream Wake Generators in a Transonic Compressor Stage Gregory Bloch, James Loellbach, Chunill Hah American Society of Mechanical Engineers
4 Technical Paper Flow analyses in a single-stage propulsion pump Lee, Yu-Tai, Hah, Chunill, Loellbach, James The American Society of Mechanical Engineers	10 Conference Proceedings Unsteady Hydrodynamic Performance Prediction of Ducted Propeller Based on CFD Ou, Li Jian, Wu, Nan Huo, Li, De Yu Trans Tech Publications
5 Technical Paper Analysis of transonic flow fields inside a high pressure ratio centrifugal compressor at design and off design conditions Hah, Chunill, Krain, Hartmut The American Society of Mechanical Engineers	11 Conference Proceedings Interaction of Rotor and Casing Treatment Flow in an Axial Single-Stage Transonic Compressor With Circumferential Grooves Martin W. Müller, Christoph Biela, Heinz-Peter Schiffer, Chunill Hah American Society of Mechanical Engineers
6 Technical Paper Unsteady Behavior of a Tip Leakage Vortex Produced by Simulated Stator/Rotor Interaction Ma, Ruolong, Saha, Nilanjan, Devenport, William J., Wang, Yu American Institute of Aeronautics and Astronautics	12 Technical Paper A viscous flow study of shock-boundary layer interaction, radial transport, and wake development in a transonic compressor Hah, Chunill, Reid, Lonnie The American Society of Mechanical Engineers

1

2

3

4

5

6

7

8

9

10

11

12