International Journal of Aerospace Engineering / 2012 / Article / Tab 1

Research Article

Assessment of Combustor Working Environments

Table 1

Engine operating conditions.

Flow parameters

Takeoff Air inlet total pressure (kPa)1000
Air mass flow rate (kg/s)2.36
Air inlet temperature (K)606
Fuel mass flow rate (kg/s)0.053

Cruise Air inlet total pressure (kPa)463
Air mass flow rate (kg/s)1.17
Air inlet temperature (K)552
Fuel mass flow rate (kg/s)0.0207