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Researcher Details
 
Name: Professor WN Dawes
Organisation: University of Cambridge
Department: Engineering
Current EPSRC-Supported Research Topics:

Current EPSRC Support
There is no current EPSRC Support
Previous EPSRC Support
EP/H004505/1 Sandpit: Airport Environmental Investment Toolkit(P)
EP/G027633/1 CAMBRIDGE UGTP WHOLE ENGINE COMPUTATIONAL AEROACOUSTICS CONSORTIUM(C)
EP/G006164/1 Commercialisation of P3: Signposting - design process modelling and simulation software(C)
EP/D060001/1 A Highly Modular Systems Model For Integrated Assessment Of Aircraft Emissions(C)
EP/D035031/1 Mathematical Modelling and Computational Engineering Prediction of Turbomachinery Broadband Noise(C)
GR/S21014/01 DARP: Unsteady Aerodynamics Prediction and Simulation for Airframe and Turbomachinery Applications (PUMA) DARP(C)
GR/R28935/01 Mathematical Modelling Myocardial Conduction and Its Relationship To Sudden Arrhythmic Death(P)
GR/N33997/01 THE RELATIONSHIP BETWEEN HEAT TRANSFER & AERODYNAMICS FOR FILM-COOLED AXIAL TURBINE TIP-CLEARANCE FLOW(C)
GR/N21901/01 A MEMS-BASED MULTI-SENSOR PROBE FOR MEASUREMENT OF THREE-DIMENSIONAL AND HIGH FREQUENCY UNSTEADY FLOWS(C)
GR/M94977/01 THERMAL MANAGEMENT OF HIGH POWER ELECTRONICS WITH LATTICE-FRAME MATERIALS(C)
GR/M85791/01 DARP: DEVELOPMENT OF PREDICTION METHODS FOR TURBINE BLADE HEAT TRANSFER & FILM COOLING FLOWS(P)
GR/M84343/01 DARP: SHOCK BOUNDARY LAYER INTERACTION: DIRECT SIMULATION & EXPERIMENT(C)
GR/L18570/02 DIRECT NUMERICAL SIMULATION & MODELLING OF TURBULANCE IN TRAILING-EDGE FLOWS(C)
GR/M05843/01 PREDICTING WAKE-PASSING TRANSITION IN TURBOMACHINERY USING AN INTERMITTENCY-CONDITIONED MODELLING APPROACH(C)
GR/L85473/01 (JREI)APPLICATION OF LASER DOPPLER ANEMOMETRY TO TURBOMACHINERY EXTERNAL AERODYNAMIC & COMBUSTION FLOWS(C)
GR/L68346/01 IMPROVING PREDICTIVE CAPABILITY OF POROSITY/ DISTRIBUTED RESISTANCE MODELS FOR CONFINED EXPLOSIONS(C)
GR/L18570/01 DIRECT NUMERICAL SIMULATION & MODELLING OF TURBULANCE IN TRAILING-EDGE FLOWS(C)
GR/H18746/01 THE AERODYNAMICS OF PLATFORM COOLANT EJECTION IN AXIAL FLOW TURBINES(C)
GR/F24696/01 THE AERODYNAMICS OF LOW ASPECT RATIO TURBINES(C)
Key: (P)=Principal Investigator, (C)=Co-Investigator, (R)=Researcher Co-Investigator