Cruising Performance - Aircraft with Mixed Power Plants Online Exam Quiz
Cruising Performance - Aircraft with Mixed Power Plants GK Quiz. Question and Answers related to Cruising Performance - Aircraft with Mixed Power Plants. MCQ (Multiple Choice Questions with answers about Cruising Performance - Aircraft with Mixed Power Plants
An aircraft is climbing with a 20? of climb angle and a 5? of angle of attack having a mass of 11,000 kg and aircraft drag is 9,000 N then determine aircraft lift.
Options
A : 11453.17 N
B : 9220.07 N
C : 11553.17 N
D : 97385.85 N
An aircraft is climbing with a 20? of climb angle and a 5? of angle of attack having a mass of 11,000 kg and aircraft drag is 9,000 N then determine engine thrust.
Options
A : 5257.79 N
B : 1810.97 N
C : 28013.99 N
D : 46082.75 N
An aircraft is climbing with a 20? of climb angle and a 5? of angle of attack having a mass of 11,000 kg and aircraft thrust is 46082.75N then determine aircraft drag.
Options
A : 33898.64 N
B : 52708.59 N
C : 82814.78 N
D : 8999.99 N
ESPH is the combination of thrust output and shaft power output.
Options
A : TRUE
B : FALSE
C : -
D : -
In cruise performance the aircraft is considered to be steady, level, straight, symmetric flight with uniform acceleration.
Options
A : TRUE
B : FALSE
C : -
D : -
The calculations in turboprop aircraft are done in a continuous function.
Options
A : TRUE
B : FALSE
C : -
D : -
The expression of range and endurance is written in terms of endurance factor and relative speed function.
Options
A : TRUE
B : FALSE
C : -
D : -
The proportions of thrust and power are independent of speed and engine output.
Options
A : TRUE
B : FALSE
C : -
D : -
What is a trim in aircraft performance?
Options
A : The state of equilibrium where the forces and moments are balanced
B : The state of equilibrium where the forces and moments are not balanced
C : The state of equilibrium where only the forces are balanced
D : The state of equilibrium where only the moments are balanced
What is the full form of ESHP?
Options
A : Equivalent shaft horsepower
B : Equal shaft horsepower
C : Engine shaft horsepower
D : Endurance shaft horsepower
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