Nehru Institute of Technology Autonomous Approved by AICTE New Delhi Affiliated to Anna University Chennai Accredited by NAAC with A NBA Accredited AERO CSE Recognized by UGC with Section 2 f U23AE201 Fundamentals of Aeronautical Engineering Question Bank Multiple Choice Questions One Mark Questions 50 Nos 1 Who is the founder of Science of Aerodynamics in 1799 2 Who separate the four forces acting on the flight vehicle 3 Who build the first successful aircraft in 1903 A Albert Williams B Sir George Cayley C Williams Rabert D Otto Lilienthal A Albert Williams B Sir George Cayley C Williams Rabert D Otto Lilienthal A Wright Brothers B Santos Dumont C Otto Lilienthal D Albert Williams A Wright Brothers B Santos Dumont C Otto Lilienthal D Williams Rabert 4 Ornithopter concept was created by 5 Who add power plant to glider design A Samuel Langely B Wright Brothers C Otto Lilienthal D Santos Dumont 6 Power driven aircraft is under A Lighter than Air B Heavier than Air 1 Page Vision To be leading Institution in Academic excellence Multidisciplinary Research Innovation Entrepreneurship and Industry relation in order to mould true citizens of the country Mission To create innovative and vibrant young leaders in Engineering and Technology field for building India as a knowledge power by improving the teaching learning process To enhance employability entrepreneurship and to improve the research competence to address Societal needs To generate engineering graduates who use knowledge as a powerful tool to drive societal transformation and inculcate in them ethical and moral values Nehru Institute of Technology Autonomous Approved by AICTE New Delhi Affiliated to Anna University Chennai Accredited by NAAC with A NBA Accredited AERO CSE Recognized by UGC with Section 2 f 7 Free balloon is under A Lighter than Air B Heavier than Air 8 Ornithopter is under A Lighter than Air B Heavier than Air 9 Flap is fixed in A Tail B Wing C Fuselage D Landing Gear 10 Rudder is A Vertical Stabilizer B Horizontal Stabilizer C Fuselage Controller D Electronic Controller 11 Elevator is A Vertical Stabilizer B Electronic Controller C Horizontal Stabilizer D Fuselage Controller 12 Engine fixed in A Fuselage B Tail Unit C Wing D Rudder 13 Primary control surface is A Rudder B Wing C Flap D Elevator 2 Page Vision To be leading Institution in Academic excellence Multidisciplinary Research Innovation Entrepreneurship and Industry relation in order to mould true citizens of the country Mission To create innovative and vibrant young leaders in Engineering and Technology field for building India as a knowledge power by improving the teaching learning process To enhance employability entrepreneurship and to improve the research competence to address Societal needs To generate engineering graduates who use knowledge as a powerful tool to drive societal transformation and inculcate in them ethical and moral values Nehru Institute of Technology Autonomous Approved by AICTE New Delhi Affiliated to Anna University Chennai Accredited by NAAC with A NBA Accredited AERO CSE Recognized by UGC with Section 2 f 14 Secondary control surface is A Rudder B Wing C Flap D Elevator 15 Trim Tab is A Primary Control Surface B Secondary Control Surface 16 Vertical speed indicator is used to determine the A Climbing and Descending B Height of an Airplane C Speed of an Airplane D Volume of an Airplane 17 Altimeter is used to determine the A Climbing and Descending B Height of an Airplane C Speed of an Airplane D Volume of an Airplane 18 Airspeed indicator is used to determine the A Static Pressure Impact Pressure B Height of an Airplane C Speed of an Airplane D Volume of an Airplane 19 Pitching control means A to turn left right B to turn up down C to roll D to revolve 20 Yawing Control surface A to turn left right B to turn up down C to roll D to revolve 3 Page Vision To be leading Institution in Academic excellence Multidisciplinary Research Innovation Entrepreneurship and Industry relation in order to mould true citizens of the country Mission To create innovative and vibrant young leaders in Engineering and Technology field for building India as a knowledge power by improving the teaching learning process To enhance employability entrepreneurship and to improve the research competence to address Societal needs To generate engineering graduates who use knowledge as a powerful tool to drive societal transformation and inculcate in them ethical and moral values Nehru Institute of Technology Autonomous Approved by AICTE New Delhi Affiliated to Anna University Chennai Accredited by NAAC with A NBA Accredited AERO CSE Recognized by UGC with Section 2 f 21 Rudder controls A Lateral Stability B Directional Stability C Longitudinal Stability D Neutral 22 Aileron controls A Lateral Stability B Directional Stability C Longitudinal Stability D Neutral 23 Elevator controls A Lateral Stability B Directional Stability C Longitudinal Stability D Neutral 24 Subsonic A M 0 8 B 0 8 1 2 C M 1 D M 5 25 Supersonic A M 0 8 B 0 8 1 2 C 1 2 5 D M 5 26 Hypersonic A M 0 8 B 0 8 1 2 C M 1 D M 5 27 Troposphere up to A 16Km B 51Km C 85Km D 600Km 4 Page Vision To be leading Institution in Academic excellence Multidisciplinary Research Innovation Entrepreneurship and Industry relation in order to mould true citizens of the country Mission To create innovative and vibrant young leaders in Engineering and Technology field for building India as a knowledge power by improving the teaching learning process To enhance employability entrepreneurship and to improve the research competence to address Societal needs To generate engineering graduates who use knowledge as a powerful tool to drive societal transformation and inculcate in them ethical and moral values Nehru Institute of Technology Autonomous Approved by AICTE New Delhi Affiliated to Anna University Chennai Accredited by NAAC with A NBA Accredited AERO CSE Recognized by UGC with Section 2 f 28 Stratosphere up to 29 Mesosphere up to A 16Km B 51Km C 85Km D 600Km A 16Km B 51Km C 85Km D 600Km A 16Km B 51Km C 85Km D 600Km A 16Km B 51Km C 85Km D 500Km 31 Exosphere up to 30 Thermosphere up to 32 Lift is a A Forward motion B Backward motion C Downward motion D Upward motion 33 Drag is a A Forward motion B Backward motion C Downward motion D Upward motion 5 Page Vision To be leading Institution in Academic excellence Multidisciplinary Research Innovation Entrepreneurship and Industry relation in order to mould true citizens