# 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

Options

A : TRUE

B : FALSE

C : -

D : -

Options

A : TRUE

B : FALSE

C : -

D : -

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

Options

A : TRUE

B : FALSE

C : -

D : -

Options

A : TRUE

B : FALSE

C : -

D : -

Options

A : 3.33

B : 0.3

C : 33.33

D : 0.333

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

Overview of an Aircraft-2

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