Thrust Weight Ratio-2 Online Exam Quiz
Thrust Weight Ratio-2 GK Quiz. Question and Answers related to Thrust Weight Ratio-2. MCQ (Multiple Choice Questions with answers about Thrust Weight Ratio-2
A jet aircraft has maximum lift to drag as 12. Find the value of the thrust loading at the cruise.
Options
A : 0.096
B : 0.0069
C : 0.96
D : 0.0096
A twin turbo prop is flying with power loading of 12. What will be the maximum velocity?
Options
A : 48.225 mph
B : 48.225 m/s
C : 48.225 km/h
D : 225.48 m/h
A typical jet airliner has cruise thrust to weight ratio of 0.5. Determine at which aerodynamic efficiency this airliner is flying.
Options
A : 2
B : 3
C : 4
D : 5
An A/C is cruising with thrust to weight of 0.9. If A/C is powered by prop engine then, find maximum lift to drag?
Options
A : 1.11
B : 2.11
C : 3.12
D : 4.221
An A/C is flying with thrust loading at take-off is 0.9. If thrust at take-off and cruse is equal then, determine the thrust loading during cruise.
Options
A : 0.941
B : 0.951
C : 0.961
D : 0.98
Based on existing engine or based on new design, aircraft sizing can be done.
Options
A : TRUE
B : FALSE
C : -
D : -
Consider thrust is given as 120 N of force then, find the value of thrust in terms of pound of force.
Options
A : 26.97 pound of force
B : 125 pound
C : 12.56 lb
D : 120 KN
Existing engine used for sizing is called as __
Options
A : fixed engine
B : unfixed engine
C : differential engine
D : rubber engine
For an aircraft cruise aerodynamic efficiency is 10. Find the thrust loading at cruise.
Options
A : 0.1
B : 0.01
C : 0.4
D : 0.5
If weight of an aircraft is increased then, thrust loading will ___
Options
A : increase
B : decrease
C : will not change
D : exact half always
Aerodynamic Coefficients more Online Exam Quiz
Structures - Material Selection and Properties