Experimental and Numerical Study on Oxidation Deposition Properties of Aviation Kerosene

Engineering

• Numerical Study 100%
• Determines 100%
• Deposition Rate 100%
• Reynolds' Number 50%
• Experimental Result 50%
• Three-Dimensional Models 50%
• Physical Parameter 50%
• Flow Condition 50%
• Temperature Time 50%
• Heat Exchanger 50%
• Micrograph 50%
• Coupling Effect 50%
• Heating Time 50%
• Surface Element 50%
• Continuous Phase 50%
• Local Heat Transfer 50%
• Deposition Mechanism 50%
• Profile Parameter 50%
• Couplings 50%
• Heat Transfer 50%
• Turbulent Flow 50%
• Fluid Viscosity 50%
• Temperature Distribution 50%
• Numerical Model 50%
• Heat Flux 50%
• Cooling System 50%
• Oxygen Consumption 50%

Keyphrases

• Aviation Kerosene 100%
• Wall Temperature Distribution 50%
• Local Heat Transfer Characteristics 50%
• Dissolved Oxygen Consumption 50%
• Local Position 50%
• Experimental Heating 50%
• Supercritical Pressure 50%
• Profile Parameters 50%
• Heat Deposition 50%
• Physicochemical Forms 50%

Chemical Engineering

• Deposition Rate 100%
• Dissolved Oxygen 50%
• Temperature Distribution 50%
• Heat Flux 50%
• Specific Heat 50%