ASE 306 PROPULSION SYSTEMS
Term Project
Due date: 30 May 2023 12:00
1. Plot Ideal Cycle showing all the stations of the engine F100-PW-100 with free stream Mach
number (Mo) of 0.8 for the sea level (SL) conditions and cruising altitude of Alt=10000m using
standard atmosphere.
2. Calculate the thrust and specific fuel consumption of the engine for above defined conditions
with afterburner on and off conditions.
3. Calculate the thrust and specific fuel consumption of the engine for above defined conditions
with afterburner on and off conditions.
4. For a mission starting from ground SL, taxi and takeoff (AB/on), climb with 100 m/s ascend
speed to altitude of 10000 m, M=0.8 (AB/off), Level flight 10 minutes and start landing with
10 m/s descend speed, with idle and landing with thrust reversal of 40% of ideal thrust and
taxi stop. Calculate and plot;
a. Thrust and Fuel consumption rate vs time.
b. Total quantity of fuel consumed.
c. Stations temperature, pressure vs time
d. Discuss the results obtained regarding to the ideal conditions, efficiencies and offdesign conditions. Compare with the technology levels.
5. Use the necessary data provided in your book. Select your fuel and use f (fuel to air ratio) for
throttling. Clearly state your assumptions during your mission such as constant drag or weight
of A/C etc where needed.
6. Write down all the equations you use in your report and explain your solution algorithm and
provide soft copy as an attachment.