Power Producing Power Plant Online Exam Quiz

Power Producing Power Plant GK Quiz. Question and Answers related to Power Producing Power Plant. MCQ (Multiple Choice Questions with answers about Power Producing Power Plant

Cruise method 1 is ideal for troposphere.

Options

A : TRUE

B : FALSE

C : -

D : -

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Minimum range is given when the aircraft is fly's at u=1.316.

Options

A : TRUE

B : FALSE

C : -

D : -

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Relative airspeed acts as a shaping factor.

Options

A : TRUE

B : FALSE

C : -

D : -

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What is endurance factor?

Options

A : \big[\frac{E_{max}}{C}\big]

B : \big[\frac{E_{max}}{VC}\big]

C : \big\{\frac{2u^3}{u^4+1}\big\}

D : \big\{\frac{2u^4}{u^4+1}\big\}

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What is endurance function?

Options

A : \big[\frac{E_{max}}{C}\big]

B : ln?

C : \big\{\frac{2u^2}{u^4+1}\big\}

D : \big\{\frac{2u^2}{u^4+1}\big\}ln?

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What is meant by static thrust?

Options

A : thrust at maximum airspeed

B : power at zero airspeed

C : thrust at zero airspeed

D : power at maximum airspeed

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What is the propeller advance ratio for the power-producing powerplant when the true airspeed is 300m/s and the diameter of propeller is 0.5 m with rotational speed of 117.81rad/sec?

Options

A : 7.01

B : 9.02

C : 5.09

D : 5.89

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Which of the following is correct statement regarding cruise method 1?

Options

A : Fuel ratio for very long range aircraft is 1.3

B : Fuel ratio for short range aircraft is 1.3

C : Fuel ratio for medium to long range aircraft is 1.3

D : Fuel ratio for short range aircraft is 1.5

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Which of the following is the correct equation for longitudinal performance equation of motion?

Options

A : \frac{\eta P}{V}=D-Wsin?2+mV

B : \frac{\eta P}{V}=D+Wsin?2-mV

C : \frac{\eta T}{V}=D+Wsin?2+mV

D : \frac{\eta P}{V}=D+Wsin?2+mV

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Which of the following relations are correct for pressure coefficient?

Options

A : CP=\frac{P}{\frac{\rho n^3D^4}{2}}

B : CP=\frac{P}{\frac{\rho n^2D^5}{2}}

C : CP=\frac{TV}{\frac{\rho n^3D^5}{2}}

D : CP=\frac{P}{\frac{\rho n^3D^5}{2}}

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Aerodynamic Relationships more Online Exam Quiz

Measurement of Height

Measurement of Mach Number

Minimum Drag Speed

Minimum Fuel Climb

Minimum Power Speed

Range and Endurance for Aircraft with Power Producing Engines

Range and Endurance for Aircraft with Thrust Producing Engines

Standard Atmospheric Model

Take-off Performance

Thrust Producing Power Plant - 1