Question: Which of the following is correct for horsepower (hp) to the weight ratio?
Options
A : T/W = (550*? / V) * (hp/W)
B : T/W = (550*? / V)
C : T/W = (550*? / V) + (hp/W)
D : T/W = (550*? / V) ? (hp/W)
Click to view Correct Answer
Thrust Weight Ratio-1 more questions
Power loading of a prop driven aircraft is defined as....
Power loading of prop driven aircraft is __
Thrust loading during flight does not remain constant as ___
Thrust to weight ratio of all the aircrafts is same.
Typically, designer designs thrust loading based on __
Wing and airfoil both are 3D phenomena.
A jet aircraft has maximum lift to drag as 12.....
A twin turbo prop is flying with power loading of....
A typical jet airliner has cruise thrust to weight ratio....
An A/C is cruising with thrust to weight of 0.9.....
Aerodynamic Coefficients more Online Exam Quiz
Structural-Analysis Fundamentals