Biography
Kam Chana joined the University in 2010 following 22 years at the MoD and QinetiQ where he held the position Head of Instrumentation & Experimental Programmes and was a QinetiQ Fellow. He held a Visiting Fellow position at Warwick University for over 20 years and a Visiting Fellow position at Surrey University. Kam has also held the position Scientific Director of the European Virtual Institute for Gas Turbine Instrumentation (EVI-GTI) for 5 years.
At Oxford he leads the activities of the Oxford Turbine Research Facility. He has over 100 peer-reviewed published articles and several patents.
Most Recent Publications
Nick N, Kirkup J, Allen M and Chana K. Thermal Product Sensing: Simulations and Experiments of a Novel Biosensor for Quantitative Thermal Property Measurement of Biological Tissues. Mega J Case Rep. 2025;8(6):2001-2019.
Nick N, Kirkup J, Allen M and Chana K. Thermal Product Sensing: Simulations and Experiments of a Novel Biosensor for Quantitative Thermal Property Measurement of Biological Tissues. Mega J Case Rep. 2025;8(6):2001-2019.
Machine Learning Classification of Skin Lesions Using Thermal Product Biosensing: A Preliminary Diagnostic Approach
Machine Learning Classification of Skin Lesions Using Thermal Product Biosensing: A Preliminary Diagnostic Approach
Development of a Novel Thermal Technique for Detection of Water in Solvents
Development of a Novel Thermal Technique for Detection of Water in Solvents
AN AERODYNAMIC INVESTIGATION OF A HIGH-PRESSURE TURBINE USING ROTOR CASING STATIC PRESSURE MEASUREMENTS AT ENGINE REPRESENTATIVE CONDITIONS WITH DIFFERENT TIP DESIGNS, TIP GAPS AND INLET TEMPERATURE PROFILES
AN AERODYNAMIC INVESTIGATION OF A HIGH-PRESSURE TURBINE USING ROTOR CASING STATIC PRESSURE MEASUREMENTS AT ENGINE REPRESENTATIVE CONDITIONS WITH DIFFERENT TIP DESIGNS, TIP GAPS AND INLET TEMPERATURE PROFILES
An aerodynamic investigation of a high-pressure turbine using rotor casing static pressure measurements at engine representative conditions with different tip designs, tip gaps and inlet temperature profiles
An aerodynamic investigation of a high-pressure turbine using rotor casing static pressure measurements at engine representative conditions with different tip designs, tip gaps and inlet temperature profiles
Research Interests
- Turbine heat transfer
- Cooling systems
- Gas turbines
- Internal combustion engine instrumentation
- Tip timing
- Tip clearance measurement
- High temperature instrumentation
Research Groups
Most Recent Publications
Nick N, Kirkup J, Allen M and Chana K. Thermal Product Sensing: Simulations and Experiments of a Novel Biosensor for Quantitative Thermal Property Measurement of Biological Tissues. Mega J Case Rep. 2025;8(6):2001-2019.
Nick N, Kirkup J, Allen M and Chana K. Thermal Product Sensing: Simulations and Experiments of a Novel Biosensor for Quantitative Thermal Property Measurement of Biological Tissues. Mega J Case Rep. 2025;8(6):2001-2019.
Machine Learning Classification of Skin Lesions Using Thermal Product Biosensing: A Preliminary Diagnostic Approach
Machine Learning Classification of Skin Lesions Using Thermal Product Biosensing: A Preliminary Diagnostic Approach
Development of a Novel Thermal Technique for Detection of Water in Solvents
Development of a Novel Thermal Technique for Detection of Water in Solvents
AN AERODYNAMIC INVESTIGATION OF A HIGH-PRESSURE TURBINE USING ROTOR CASING STATIC PRESSURE MEASUREMENTS AT ENGINE REPRESENTATIVE CONDITIONS WITH DIFFERENT TIP DESIGNS, TIP GAPS AND INLET TEMPERATURE PROFILES
AN AERODYNAMIC INVESTIGATION OF A HIGH-PRESSURE TURBINE USING ROTOR CASING STATIC PRESSURE MEASUREMENTS AT ENGINE REPRESENTATIVE CONDITIONS WITH DIFFERENT TIP DESIGNS, TIP GAPS AND INLET TEMPERATURE PROFILES
An aerodynamic investigation of a high-pressure turbine using rotor casing static pressure measurements at engine representative conditions with different tip designs, tip gaps and inlet temperature profiles
An aerodynamic investigation of a high-pressure turbine using rotor casing static pressure measurements at engine representative conditions with different tip designs, tip gaps and inlet temperature profiles
