MCQOPTIONS
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MCQOPTIONS
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. | \(\big[\frac{\lambda}{u}+τ\big]+\frac{1}{2}\big[u^2+\frac{1}{u^2}\big]\)=Emax\(\big\{sin\gamma_2-\frac{V}{g}\big\}\) |
| B. | \(\big[\frac{\lambda}{u}+τ\big]-\frac{1}{2}\big[u^2+\frac{1}{u^2}\big]\)=Emax\(\big\{sin\gamma_2-\frac{V}{g}\big\}\) |
| C. | \(\big[\frac{\lambda}{u}+τ\big]+\frac{1}{2}\big[u^2+\frac{1}{u^2}\big]\)=Emax\(\big\{sin\gamma_2+\frac{V}{g}\big\}\) |
| D. | \(\big[\frac{\lambda}{u}+τ\big]-\frac{1}{2}\big[u^2+\frac{1}{u^2}\big]\)=Emax\(\big\{sin\gamma_2+\frac{V}{g}\big\}\) |
| 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. | Vmp=\(\frac{1}{\sqrt[2]{3}}\)Vmd |
| B. | Vmp=\(\frac{1}{\sqrt[4]{3}}\)Vmd |
| C. | Vmp=\(\frac{1}{\sqrt[3]{3}}\)Vmd |
| D. | Vmp=\(\frac{1}{\sqrt[4]{5}}\)Vmd |
| Answer» C. Vmp=\(\frac{1}{\sqrt[3]{3}}\)Vmd | |
| 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. \(\big(\frac{2W}{\gamma \rho S}\big)^{\frac{1}{2}}\big(\frac{K}{C_{Dz}}\big)^\frac{1}{4}\) | |