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Results: 1-10 |
Results: 10
ON THE INTERPRETATION OF MEASURED PROFILE LOSSES IN UNSTEADY WAKE - TURBINE BLADE INTERACTION STUDIES
Authors: HODSON HP DAWES WN
Citation: Hp. Hodson et Wn. Dawes, ON THE INTERPRETATION OF MEASURED PROFILE LOSSES IN UNSTEADY WAKE - TURBINE BLADE INTERACTION STUDIES, Journal of turbomachinery, 120(2), 1998, pp. 276-284
A SOLUTION-ADAPTIVE MESH PROCEDURE FOR PREDICTING CONFINED EXPLOSIONS
Authors: WATTERSON JK CONNELL IJ SAVILL AM DAWES WN
Citation: Jk. Watterson et al., A SOLUTION-ADAPTIVE MESH PROCEDURE FOR PREDICTING CONFINED EXPLOSIONS, International journal for numerical methods in fluids, 26(2), 1998, pp. 235-247
AERODYNAMIC ASPECTS OF ENDWALL FILM-COOLING
Authors: FRIEDRICHS S HODSON HP DAWES WN
Citation: S. Friedrichs et al., AERODYNAMIC ASPECTS OF ENDWALL FILM-COOLING, Journal of turbomachinery, 119(4), 1997, pp. 786-793
DISTRIBUTION OF FILM-COOLING EFFECTIVENESS ON A TURBINE ENDWALL MEASURED USING THE AMMONIA AND DIAZO TECHNIQUE
Authors: FRIEDRICHS S HODSON HP DAWES WN
Citation: S. Friedrichs et al., DISTRIBUTION OF FILM-COOLING EFFECTIVENESS ON A TURBINE ENDWALL MEASURED USING THE AMMONIA AND DIAZO TECHNIQUE, Journal of turbomachinery, 118(4), 1996, pp. 613-621
COMPUTATIONAL STUDY OF VISCOUS EFFECTS ON LOBED MIXER FLOW FEATURES AND PERFORMANCE
Authors: OSULLIVAN MN KRASNODEBSKI JK WAITZ IA GREITZER EM TAN CS DAWES WN
Citation: Mn. Osullivan et al., COMPUTATIONAL STUDY OF VISCOUS EFFECTS ON LOBED MIXER FLOW FEATURES AND PERFORMANCE, Journal of propulsion and power, 12(3), 1996, pp. 449-456
A SIMULATION OF THE UNSTEADY INTERACTION OF A CENTRIFUGAL IMPELLER WITH ITS VANED DIFFUSER - FLOW-ANALYSIS
Authors: DAWES WN
Citation: Wn. Dawes, A SIMULATION OF THE UNSTEADY INTERACTION OF A CENTRIFUGAL IMPELLER WITH ITS VANED DIFFUSER - FLOW-ANALYSIS, Journal of turbomachinery, 117(2), 1995, pp. 213-222
A NUMERICAL INVESTIGATION OF AEROFOIL BOUNDARY-LAYER MANIPULATOR PROFILE FOR CRUISE-FLIGHT CONDITIONS
Authors: HUSTAD CW SAVILL AM DAWES WN
Citation: Cw. Hustad et al., A NUMERICAL INVESTIGATION OF AEROFOIL BOUNDARY-LAYER MANIPULATOR PROFILE FOR CRUISE-FLIGHT CONDITIONS, Applied scientific research, 54(4), 1995, pp. 267-280
THE SOLUTION-ADAPTIVE NUMERICAL-SIMULATION OF THE 3-DIMENSIONAL VISCOUS-FLOW IN THE SERPENTINE COOLANT PASSAGE OF A RADIAL INFLOW TURBINE BLADE
Authors: DAWES WN
Citation: Wn. Dawes, THE SOLUTION-ADAPTIVE NUMERICAL-SIMULATION OF THE 3-DIMENSIONAL VISCOUS-FLOW IN THE SERPENTINE COOLANT PASSAGE OF A RADIAL INFLOW TURBINE BLADE, Journal of turbomachinery, 116(1), 1994, pp. 141-148
A COMPARISON OF THE MEASURED AND PREDICTED FLOW FIELD IN A MODERN FAN-BYPASS CONFIGURATION
Authors: GOYAL RK DAWES WN
Citation: Rk. Goyal et Wn. Dawes, A COMPARISON OF THE MEASURED AND PREDICTED FLOW FIELD IN A MODERN FAN-BYPASS CONFIGURATION, Journal of turbomachinery, 115(2), 1993, pp. 273-282
THE EXTENSION OF A SOLUTION-ADAPTIVE 3-DIMENSIONAL NAVIER-STOKES SOLVER TOWARD GEOMETRIES OF ARBITRARY COMPLEXITY
Authors: DAWES WN
Citation: Wn. Dawes, THE EXTENSION OF A SOLUTION-ADAPTIVE 3-DIMENSIONAL NAVIER-STOKES SOLVER TOWARD GEOMETRIES OF ARBITRARY COMPLEXITY, Journal of turbomachinery, 115(2), 1993, pp. 283-295
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