Aerodynamic Relationships Online Exam Quiz
Aerodynamic Relationships GK Quiz. Question and Answers related to Aerodynamic Relationships. MCQ (Multiple Choice Questions with answers about Aerodynamic Relationships
Airspeed with minimum power speed relates to the performance of the aircraft with power producing engine.
Options
A : TRUE
B : FALSE
C : -
D : -
Gravitational force is the product of mass of the aircraft and its acceleration.
Options
A : TRUE
B : FALSE
C : -
D : -
In a glider the engine used is thrust producing engine.
Options
A : TRUE
B : FALSE
C : -
D : -
In which of the following terms the forces of aircraft must be considered?
Options
A : Aircraft weight, flight mach number, altitude
B : Aircraft weight, airspeed, altitude, temperature
C : Aircraft weight, flight mach number, temperature
D : Aircraft weight, airspeed, altitude
Inertial forces from the mass of the aircraft and its acceleration.
Options
A : TRUE
B : FALSE
C : -
D : -
The aerodynamic forces arise from the relative motion between the aircraft and the air mass in which it is flying.
Options
A : TRUE
B : FALSE
C : -
D : -
What is the relative airspeed of an aircraft whose airspeed and minimum drag speed are 500m/s and 150m/s?
Options
A : 3.33
B : 0.3
C : 33.33
D : 0.333
What will be the drag to minimum drag ratio when the relative airspeed is 3.33?
Options
A : 5.49
B : 1.51
C : 5.59
D : 1.82
Which of the following is the correct performance equation?
Options
A : \big[\frac{\lambda}{u}+?\big]+\frac{1}{2}\big[u^2+\frac{1}{u^2}\big]=Emax\big\{sin\gamma_2-\frac{V}{g}\big\}
B : \big[\frac{\lambda}{u}+?\big]-\frac{1}{2}\big[u^2+\frac{1}{u^2}\big]=Emax\big\{sin\gamma_2-\frac{V}{g}\big\}
C : \big[\frac{\lambda}{u}+?\big]+\frac{1}{2}\big[u^2+\frac{1}{u^2}\big]=Emax\big\{sin\gamma_2+\frac{V}{g}\big\}
D : \big[\frac{\lambda}{u}+?\big]-\frac{1}{2}\big[u^2+\frac{1}{u^2}\big]=Emax\big\{sin\gamma_2+\frac{V}{g}\big\}
Aerodynamic Relationships more Online Exam Quiz
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