Investigation of the flowfield in the transonic VKI BRITE EURAM turbine stage with 3D steady and unsteady N-S computations

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 2000, Pages

  Laumert, Björn ^a,b   Mårtensson, Hans ^a   Fransson, Torsten H ^b  

^a VOLVO AERO CORPORATION   (Sweden)

^b ROYAL INSTITUTE OF TECHNOLOGY   (Sweden)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT ENGINES; FIGHTER AIRCRAFT; GEOMETRY; NAVIER STOKES EQUATIONS; ROTORS (WINDINGS); STATORS; SUPERSONIC AIRCRAFT; TURBINES; TURBOMACHINE BLADES;

COOLING FLOWS; NAVIER-STOKES COMPUTATIONS; PRESSURE PERTURBATION; PRESSURE SIDE; THREEDIMENSIONAL (3-D); TRAILING EDGE GEOMETRIES; TRAILING EDGES; TURBINE STAGES;

GAS TURBINES;

EID: 84955273350     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0433     Document Type: Conference Paper

References (10)

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7. Michelassi, V, Martelli, E, Denos, R., Arts, T., Sieverding, C.H., 1998, "Unsteady heat transfer in stator-rotor interaction by two equation turbulence model", ASME paper 98-GT-243
8. Moss, R. W., Ainsworth, R. W., Sheldrake, C. D. and Miller, R. 1997, "The unsteady pressure field over a turbine blade surface: visualization and interpretation of experimental data", ASME paper 97-GT-474
9. Saxer, A. P., Giles, M. B., 1994, "Predictions of three-dimensional steady and unsteady inviscid transonic stator/rotor interaction with inlet radial temperature nonuniformity", ASME Journal of Turbomachinery, Vol. 116, pp. 347-357
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