GUJARAT TECHNOLOGICAL UNIVERSITY
BE - SEMESTER- VII (New) EXAMINATION — WINTER 2019
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Subject Code: 2170101 Date: 23/11/2019Subject Name: Aircraft Design I
Time: 10:30 AM TO 01:00 PM Total Marks: 70
Instructions:
1. Attempt all questions.
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2. Make suitable assumptions wherever necessary.3. Figures to the right indicate full marks.
4. Use drawing instruments to make figures.
MARKS
Q.1 (a) Discuss three phases of aircraft design process in one sentence. 03
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(b) Define Basic empty weight, expandable payload, reserve fuel, 04maximum zero fuel weight.
(c) Shortly explain different phases of flight of a conventional ground 07
attack aircraft.
Q.2 (a) Define all parameters required to start aircraft design. 03
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(b) Discuss various types of wing layout and their necessity. 04(c) Explain aircraft development process with block diagram. 07
OR
(c) How will you determine fuel fraction for weight estimation. 07
Q.3 (a) How will you determine Maximum Takeoff Weight after determining 03
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Fuel weight?(b) Explain effect of thrust to weight ratio on climb performance. 04
(c) Explain effect of wing loading on takeoff performance in various 07
temperature and density conditions:
OR
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Q.3 (a) Which aerodynamic considerations are required to design a 03supersonic public transport aircraft?
(b) Explain advantages and disadvantages of H-tail and V-Tail 04
configurations with neat sketch.
(c) Classify types of drag explain each of one in one sentence. 07
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Q.4 (a) How will you determine area of horizontal stabilizer of a jet transport 03
aircraft? Explain with neat sketch.
(b) Which considerations should be taken to choose airfoil section of a 04
horizontal stabilizer?
(c) How will you decide plan form shape of horizontal tail plane for 07
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different applications and airspeeds?OR
Q.4 (a) How will you determine are of vertical fin of a supersonic jet fighter 03
aircraft?
(b) Discuss considerations to place horizontal stabilizer and set a proper 04
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tail moment arm.(c) How will you select type of aircraft engine for particular design? 07
Q.5 (a) Only draw suitable locations for placements of aircraft engines 03
(b) Explain principle of optimization with examples. 04
(c) What are the considerations to select material for particular 07
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components?OR
Q.5 (a) Discuss any one type of main rotor configuration with respect to 03
maneuvering controls.
(b) What is refined weight estimation method? 04
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(c) Explain function of cyclic and collective pitch control. 07--- Content provided by FirstRanker.com ---
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