Aircraft Performance

1.7.98 Relationship between fuel flow, thrust available, thrust required and velocity for a turbojet airplane in straight and level flight

1.7.99 Relationship between fuel flow, power available, power required, and velocity for a turboprop airplane in straight and level flight

1.7.100 Define Maximum Range and Maximum Endurance

1.7.101 and 1.7.102 State the angel of attack and velocity , compared to L/D max at which turbojet and turboprops achieve maximum endurance and range