Thrust Weight Ratio-1 Online Exam Quiz
Thrust Weight Ratio-1 GK Quiz. Question and Answers related to Thrust Weight Ratio-1. MCQ (Multiple Choice Questions with answers about Thrust Weight Ratio-1
A 3D airfoil is called ___
Options
A : wing
B : airfoil
C : engine
D : lofting
A jet fighter aircraft is flying with maximum Mach number of 2.0. What will be the thrust loading of the fighter?
Options
A : 0.57
B : 0.64
C : 2.5
D : 2
A/C with higher thrust to weight ratio can accelerate more quickly.
Options
A : TRUE
B : FALSE
C : -
D : -
An aircraft is cruising with lift coefficient of 2.5 and thrust loading of 0.6. Find drag coefficient of the aircraft.
Options
A : 1.5
B : 2.5
C : 2.6
D : 2.59
Can we estimate thrust loading based on Wing loading?
Options
A : Yes
B : No
C : Both are same
D : Are not related to each other
Determine the corrections or otherwise of the following assertion [A] and reason [R]:^ Assertion [A]: Aerobatic prop aircraft has much higher power loading.^ Reason[R]: Power loading of prop aircraft is ratio of power to the weight of the aircraft.
Options
A : Both [A] and [R] are true and [R] is the correct reason for [A]
B : Both [A] and [R] are true but [R] is not the correct reason for [A]
C : Both [A] and [R] are false
D : [A] is false but [R] is true
Higher value of thrust loading indicates __
Options
A : higher maximum speed
B : lowest maximum speed
C : lowest climb
D : lowest acceleration
If a turboprop is cruising with 2275kg of weight, then determine power loading. Given power = 190hp.
Options
A : 12
B : 5
C : 10
D : 25
If thrust loading is 0.65 then, find the power loading of a prop aircraft. Consider propeller is idle.
Options
A : 846.15/V
B : 846.15
C : 650
D : 6.5
Power loading of a prop driven aircraft is defined as ___
Options
A : weight of aircraft to the horsepower by prop engine
B : weight of aircraft into the horsepower by prop engine
C : horsepower by prop engine
D : weight of aircraft
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