Range and Endurance for Aircraft with Thrust Producing Engines Online Exam Quiz
Range and Endurance for Aircraft with Thrust Producing Engines GK Quiz. Question and Answers related to Range and Endurance for Aircraft with Thrust Producing Engines. MCQ (Multiple Choice Questions with answers about Range and Endurance for Aircraft with Thrust Producing Engines
The second fuel flow law is used in the turbojet or turbofan.
Options
A : TRUE
B : FALSE
C : -
D : -
The system of forces acting on the aircraft are propulsive forces, aerodynamic forces, gravitational forces and these result in inertial forces.
Options
A : TRUE
B : FALSE
C : -
D : -
The total thrust force assumed in the derivation of equations of motion is ___
Options
A : FN=T cos?+DM
B : FN=T cos?-DM
C : T cos?=DM-FN
D : DM=T cos?+FN
There are two fuel flow laws. They are:^ i. C=C1, here specific fuel consumption is constant^ ii. C=C3+C4M, here it considers temperature and effects of mach number
Options
A : TRUE
B : FALSE
C : -
D : -
What is meant by fuel ratio?
Options
A : ratio of initial fuel of aircraft to that of final weight of aircraft
B : ratio of final fuel of aircraft to that of initial weight of aircraft
C : ratio of initial weight of aircraft to that of final weight of aircraft
D : ratio of final weight of aircraft to that of initial weight of aircraft
What is the basic assumption taken in formulating equations of motion?
Options
A : All the engines will operate at equal gross thrust
B : All the engines do not operate at equal gross thrust
C : All the engines will operate at equal gross drag
D : All the engines do not operate at equal gross drag
What is the fuel ratio of aircraft when initial and final weight are 385560kg and 15560kg?
Options
A : 34.78
B : 24.78
C : 56.76
D : 45.65
Which of the following is a correct equation?
Options
A : Fa+Fp+Fg=Fl
B : Fa+Fp+Fg=Fl
C : Fa+Fp+Fg=Fl
D : Fa+Fp+Fg=Fl
Which of the following is not the additional assumption taken in the derivation of the equations of motion?
Options
A : Gross thrust acts in aircraft body axis
B : Thrust component is small compared to lift component
C : Aircraft is in symmetric flight
D : Rate of change of mass is neglected
Aerodynamic Relationships more Online Exam Quiz
Range and Endurance for Aircraft with Power Producing Engines
Thrust Producing Power Plant - 1