Effect of Wind on Climb Performance and Descent Performance Online Exam Quiz
Effect of Wind on Climb Performance and Descent Performance GK Quiz. Question and Answers related to Effect of Wind on Climb Performance and Descent Performance. MCQ (Multiple Choice Questions with answers about Effect of Wind on Climb Performance and Descent Performance
The curly bracket in the accelerating force represents the net propulsive thrust- weight ratio.
Options
A : TRUE
B : FALSE
C : -
D : -
The horizontal component of the true airspeed is ___
Options
A : increased by tailwind
B : decreased by tailwind
C : increased by headwind
D : unaffected by the airspeed
The performance relative to ground is effected by the wind.
Options
A : TRUE
B : FALSE
C : -
D : -
The rate of climb or descent relative to air mass is unaffected by the tailwind.
Options
A : TRUE
B : FALSE
C : -
D : -
What are the additional forces acting on the aircraft?
Options
A : Runway friction
B : Lift
C : Thrust
D : Power
What is meant by perceived performance?
Options
A : Visualization of the aircraft with respect to wind
B : Visualization of the aircraft with respect to aircraft relative to ground
C : Visualization of the aircraft with respect to wind with respect to ground
D : Visualization of the aircraft with respect to any one frame such as aircraft or ground
What is wind shear?
Options
A : The extreme case of airspeed effect on the aircraft
B : The extreme case of wind effect on the aircraft
C : The extreme case of temperature effect on the wind
D : The extreme case of altitude effect on the wind
Which of the following are the correct equations for take-off run?
Options
A : FN+D-Wsin?R-?rR=mV?
B : R-L=Wcos?R
C : R-L=Wsin?R
D : FN-D-Wsin?R-?rR=mV?
Which of the following is the correct formula for accelerating force?
Options
A : \frac{F}{W}=\Big\{\frac{F_N}{W}+\mu_R-sin\gamma_R\Big\}-\frac{L}{W}\Big(\frac{C_D}{C_L}-\mu_R\Big)FW ={F N W +? R ?sin? R }?LW (C D C L ?? R )
B : \frac{F}{W}=\Big\{\frac{F_N}{W}-\mu_R+sin\gamma_R\Big\}-\frac{L}{W}\Big(\frac{C_D}{C_L}-\mu_R\Big)FW ={F N W ?? R +sin? R }?LW (C D C L ?? R )
C : \frac{F}{W}=\Big\{\frac{F_N}{W}-\mu_R-sin\gamma_R\Big\}-\frac{L}{W}\Big(\frac{C_D}{C_L}-\mu_R\Big)
D : \frac{F}{W}=\Big\{\frac{F_N}{W}-\mu_R-sin\gamma_R\Big\}-\frac{L}{W}\Big(\frac{C_D}{C_L}+\mu_R\Big)
Aerodynamic Relationships more Online Exam Quiz
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Effect on the Take-off Distances of Flight Variables
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Estimation of Take-off Distances