My Report

Aircraft Design Practice Test 1


Correct Answer: 2 points | Wrong: -1 point
Grades: A* (100% score) | A (80%-99%) | B (60%-80%) | C (40%-60%) | D (0%-40%)
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1. Estimation of take-off weight is an iterative method.

2. Can we use similar design phases for an Airplane and for a Helicopter?

3. Airfoil is a streamline shape.

4. The drawing which represents the rough idea of the actual design is called as ______

5. An aerofoil is operating with flow velocity of 100m/s. Aerofoil is symmetric and is at 0° AOA. Determine lift produced by this aerofoil.

6. Which of the following is a correct pair?

7. The three view drawing which shows arrangements of parts during conceptual design is called as _____

8. What will be the total fuel weight fraction for x-number of mission phases?

9. Variable sweep wings have higher empty weight fraction than that of the fixed sweep wing.

10. NACA stands for _____


 

Manish Bhojasia - Founder & CTO at Sanfoundry
Manish Bhojasia, a technology veteran with 20+ years @ Cisco & Wipro, is Founder and CTO at Sanfoundry. He lives in Bangalore, and focuses on development of Linux Kernel, SAN Technologies, Advanced C, Data Structures & Alogrithms. Stay connected with him at LinkedIn.

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