Performance of JP-8 unified fuel in a small bore indirect injection diesel engine for APU applications

Engineering

• Auxiliary Power Unit 100%
• Aviation Fuels 50%
• Combustion Chamber 50%
• Combustion Temperature 50%
• Compression Ratio 50%
• Continuous Operation 50%
• Convection Loss 50%
• Diesel Engine 100%
• Diesel Fuel 50%
• Engine Cylinders 50%
• Engine Performance 50%
• Heat Flux 50%
• Heat Losses 50%
• Heat Release 50%
• Ignition Delay 50%
• Indirect Injection Diesel Engine 100%
• Maximum Temperature 50%
• Mechanical Efficiency 50%
• Peak Pressure 50%
• Power Generation 50%
• Power Stroke 50%
• Room Temperature 50%