
Hypersonic Shock Tube
A modular shock tube for studying hypersonic flow physics, shock–boundary layer interaction, and high-enthalpy effects. The design emphasizes interchangeable driver/driven sections, precise diaphragm control, and optical access for schlieren and high-speed imaging.
- Driver pressures up to the designed rating (modular safety margins).
- Optical section for schlieren and chemiluminescence.
- Fast instrumentation: PCB pressure, photodiodes, trigger sync.
- CFD support for nozzle design and wall heating estimates.
Shock physics
Hypersonics
Diagnostics

Incinerator Modelling
Transient combustion and pollutant formation modelling for small-scale incinerators. The objective is to quantify ignition stability, vortex-driven mixing, and NOx/soot tendencies across operating envelopes.
- Reduced/finite-rate chemistry for practical fuels.
- Radiation and wall-heat loss modelling.
- Parametric studies for air–fuel staging and dilution.
- Validation plan via temperature/UV sensors and exhaust sampling.
Combustion
Emissions
Modeling