Question: 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
Click to view Correct Answer
Thrust Weight Ratio-1 more questions
A jet fighter aircraft is flying with maximum Mach number....
A/C with higher thrust to weight ratio can accelerate more....
An aircraft is cruising with lift coefficient of 2.5 and....
Can we estimate thrust loading based on Wing loading?
Higher value of thrust loading indicates __
If a turboprop is cruising with 2275kg of weight, then....
If thrust loading is 0.65 then, find the power loading....
Power loading of a prop driven aircraft is defined as....
Power loading of prop driven aircraft is __
Aerodynamic Coefficients more Online Exam Quiz
Structural-Analysis Fundamentals