MCQOPTIONS
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This section includes 10 Mcqs, each offering curated multiple-choice questions to sharpen your Aircraft Performance knowledge and support exam preparation. Choose a topic below to get started.
| 1. |
Which of the following is the correct performance equation? |
| A. | ( big[ frac{ lambda}{u}+ big]+ frac{1}{2} big[u^2+ frac{1}{u^2} big] )=E<sub>max</sub> ( 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] )=E<sub>max</sub> ( 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] )=E<sub>max</sub> ( 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] )=E<sub>max</sub> ( big {sin gamma_2+ frac{V}{g} big } ) |
| Answer» E. | |
| 2. |
What will be the drag to minimum drag ratio when the relative airspeed is 3.33? |
| A. | 5.49 |
| B. | 1.51 |
| C. | 5.59 |
| D. | 1.82 |
| Answer» D. 1.82 | |
| 3. |
What is the relative airspeed of an aircraft whose airspeed and minimum drag speed are 500m/s and 150m/s? |
| A. | 3.33 |
| B. | 0.3 |
| C. | 33.33 |
| D. | 0.333 |
| Answer» B. 0.3 | |
| 4. |
In a glider the engine used is thrust producing engine. |
| A. | True |
| B. | False |
| Answer» C. | |
| 5. |
Airspeed with minimum power speed relates to the performance of the aircraft with power producing engine. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 6. |
What is the value of minimum power speed when minimum drag speed is 300m/s? |
| A. | 173.21 m/s |
| B. | 227.95 m/s |
| C. | 134.16 m/s |
| D. | 200.62 m/s |
| Answer» C. 134.16 m/s | |
| 7. |
Which of the following is the correct relation between minimum power speed and minimum drag speed? |
| A. | V<sub>mp</sub>= ( frac{1}{ sqrt[2]{3}} )V<sub>md</sub> |
| B. | V<sub>mp</sub>= ( frac{1}{ sqrt[4]{3}} )V<sub>md</sub> |
| C. | V<sub>mp</sub>= ( frac{1}{ sqrt[3]{3}} )V<sub>md</sub> |
| D. | V<sub>mp</sub>= ( frac{1}{ sqrt[4]{5}} )V<sub>md</sub> |
| Answer» C. V<sub>mp</sub>= ( frac{1}{ sqrt[3]{3}} )V<sub>md</sub> | |
| 8. |
At steady state flight condition |
| A. | T>D |
| B. | T<D |
| C. | T=D |
| D. | T D |
| Answer» D. T D | |
| 9. |
The minimum drag mach number is given by ___________ |
| A. | ( big( frac{2W}{ rho S} big)^{ frac{1}{2}} big( frac{K}{C_{Dz}} big)^ frac{1}{4} ) |
| B. | ( big( frac{2W}{ gamma rho S} big)^{ frac{1}{2}} big( frac{K}{C_{Dz}} big)^ frac{1}{4} ) |
| C. | ( big( frac{2W}{ rho S} big)^{ frac{1}{2}} big( frac{K}{C_{Dz}} big)^ frac{1}{2} ) |
| D. | ( big( frac{2W}{ gamma rho S} big)^{ frac{1}{2}} big( frac{K}{C_{Dz}} big)^ frac{1}{2} ) |
| Answer» C. ( big( frac{2W}{ rho S} big)^{ frac{1}{2}} big( frac{K}{C_{Dz}} big)^ frac{1}{2} ) | |
| 10. |
The minimum drag speed is given by ___________ |
| A. | ( big( frac{2W}{ rho S} big)^{ frac{1}{2}} big( frac{K}{C_{Dz}} big)^ frac{1}{4} ) |
| B. | ( big( frac{2W}{ gamma rho S} big)^{ frac{1}{2}} big( frac{K}{C_{Dz}} big)^ frac{1}{4} ) |
| C. | ( big( frac{2W}{ rho S} big)^{ frac{1}{2}} big( frac{K}{C_{Dz}} big)^ frac{1}{2} ) |
| D. | ( big( frac{2W}{ gamma rho S} big)^{ frac{1}{2}} big( frac{K}{C_{Dz}} big)^ frac{1}{2} ) |
| Answer» B. ( big( frac{2W}{ gamma rho S} big)^{ frac{1}{2}} big( frac{K}{C_{Dz}} big)^ frac{1}{4} ) | |