Design of the blade geometry of swept transonic fans by 3D inverse design

American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI

Volumn 6 A, Issue , 2003, Pages 603-612

  Watanabe, H ^a   Zangeneh, M ^b  

^a Advanced Design Technology Ltd   (United Kingdom)

^b UNIVERSITY COLLEGE LONDON   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL FANS; PRESSURE RATIO;

COMPRESSORS; COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL GEOMETRY; INVERSE PROBLEMS; OPTIMIZATION; STATORS; TURBOMACHINE BLADES;

FANS;

EID: 0346334239     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2003-38770     Document Type: Conference Paper

References (14)

1. Adamczyk,J.J., Celestina, M.L., Greitzer, E.M., "The Role of Tip Clearance in High-Speed Fan Stall", Journal of Turbomachinery, Vol. 115, pp 28-39, 1993
2. AGARD-AR-275, "Test Cases for Computation of Internal Flows in Aero Engine Components", AGARD Advisory Report No.275, 1985.
3. Blaha,C., Kablitz, S., Hennecke, D.K., Schmidt-Eisenlohr, U., Pirker, K., Haselhoff, S., "Numerical Investigation of The Flow in an Aft-Swept Transonic Compressor Rotor", ASME Paper No. 2000-GT-0490, 2000.
4. Denton, J.D., "The Calculation of Three Dimensional Viscous Flow Through Multistage Turbomachines", ASME Paper No. 90-GT-19, 1990.
5. Denton, J.D., Xu, L., "The Effect of Lean and Sweep on Transonic Fan Performance", ASME Paper No. GT-2002-30327, 2002.
6. Gallimore, S.J., Bolger, J.J., Cumpsty, N.A., Taylor, M.J., Wright, P.I., Place, J.M.M.,"The Use of Sweep and Dihedral in Multistage Axial Flow Compressor Blading Part I: University Research and Methods Development.", ASME Paper No. GT-2002-30328, 2002.
7. Hah, C., Reid, L., "A Viscous Flow Study of Shock-Boundary Layer Interaction, Radial Transport, and Wake Development in a Transonic Compressor", Journal of Turbomachinery, Vol. 114, pp 538-547, 1992
8. Hawthorne, W.R., Tan, C.S., Wang, C. and McCune, J., "Theory of Blade Design for Large Deflections: Part I - Two Dimensional Cascades", J. of Eng. For Gas Turbine and Power, Vol.106, pp 346-353, 1984.
9. Jennions, I.K., "Three-Dimensional Navier-Stokes Computations of Transonic Fan Flow Using an Explicit Flow Solver and an Implicit k-e Solver", Journal of Turbomachinery, Vol. 115, pp 261-272, 1993
10. Sasaki, T., Breugelmans, F., "Comparison of Sweep and Dihedral Effects on Compressor Cascade Performance", ASME Paper No. 97-GT-2, 1997.
11. Wadia, A.R., Szucs, P.N., Crall, D.W., "Inner Workings of Aerodynamic Sweep", ASME Journal of Turbomachinery, Vol. 120, pp. 671-682, 1998.
12. Tiow, W.T., Zangeneh, M., "A Three Dimensional Viscous Transonic Inverse Design Method", ASME Paper No. 2000-GT-525, 2000.
13. Xing, X.Q., Zhou,S., Zhao, X.I., "Probing Into the Connotation of Sweep Aerodynamics of Transonic Fans And Compressor", ASME Paper No. 2001-GT-0352, 2001.
14. Zangeneh, M., "A Compressible Three-Dimensional Design Method for Radial and Mixed Flow Turbomachinery Blades", Int J. Numerical Methods in Fluids, Vol. 13, pp.599-624., 1991