My Report

Aircraft Design Practice Test 7


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. Let's consider we need to design avionics system for general aviation aircraft. If empty weight of aircraft is 100 unit then what will be the approximate range of required avionics weight.

2. A pneumatic subsystem is used to ______________

3. Which of the following is correct?

4. A twin business engine is designed in such way that the load of 250 unit is carried out by the tire. Find the appropriate ratio of the diameter to the width of main wheel.

5. If an airfoil is designed to provide lift curve slope as 7.8, then find airfoil efficiency. The actual lift curve slope of the airfoil is 7.4.

6. Determine the gear load factor if landing weight is 250 unit and average total load during deflection is 550 unit.

7. Following diagram represents ______
aircraft-design-questions-answers-gear-retraction-geometry-q3

8. None of the seaplanes can ever land on airfields.

9. Following diagram represents _______________
aircraft-design-questions-answers-lift-q2

10. Which of the following is a method for estimating the potato drag?


 

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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