The application of actuator disks to calculations of the flow in turbofan installations

Journal of Turbomachinery

Volumn 119, Issue 4, 1997, Pages 733-741

  Joo, W G ^a,b   Hynes, T P ^a  

^a UNIVERSITY OF CAMBRIDGE   (United Kingdom)

^b Yonsei University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATOR; FLOW; TURBOMACHINERY;

EID: 0031468756     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841183     Document Type: Article

References (6)

1. Dawes, W. N., 1988, “Development of a 3D Navier-Stokes Solver for Application to All Types of Turbomachinery,” ASME Paper No. 88-GT-70.
2. Freeman, C., and Cumpsty, N. A., 1992, “Method for the Prediction of Supersonic Compressor Blade Performance,” AIAA Journal of Propulsion, Vol. 8, pp. 199-208.
3. Ham, X. X., and Williams, Y. Y., 1983, “Flow Field Coupling Between Compression System Components,” presented at the IGTC Tokyo Conference.
4. Joo, W. G., 1994, “Intake/Engine Flow Field Coupling in Turbofan Engines,” Ph.D. Thesis, Cambridge University Engineering Department, United Kingdom.
5. Joo, W. G., and Hynes, T. P., 1997, “The Simulation of Turbomachinery Blade Rows in Asymmetric Flow Using Actuator Disks,” ASME Journal of Turbomachinery, Vol. 119, this issue, pp. 723-732.
6. Moore, F. K., 1984, “A Theory of Rotating Stall of Multistage Compressors: Part I-Small Disturbances,” ASME Journal of Engineering for Gas Turbines and Power, Vol. 106, pp. 313-320.