GATE AE Question Paper 2007 Aerospace Engineering

GATE AE Question Paper 2007 Aerospace Engineering.

GATE i.e. Graduate Aptitude Test in Engineering Aerospace Engineering 2007 Exam Has been Conducted by IISc Bangalore IIT Bombay IIT Delhi IIT Guwahati IIT Kanpur IIT Kharagpur IIT Madras IIT Roorkee. This GATE AE 2007 examination is the procedure to get the admission in M.Tech

GATE Aerospace Engineering i.e. AE Question Paper, This GATE AE 2007 Question will help all the students for their exam preparation, here the question type is MCQ i.e multiple choice question answers, if this GATE AE 2007 question paper in pdf file for GATE AE you can download it in FRAE, if GATE Aerospace Engineering 2007 paper in text for GATE AE you can download GATE AE 2007 page also just Go to menu bar, Click on File->then Save.

GATE AE Question Paper 2007 Aerospace Engineering

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Q.1 Which one of the following engines should be used by a subsonic passenger transport airplane for minimum specific fuel consumption?
(A) Turbojet engine with afterburner
(B) Turbofan engine
(C) Ramjet engine
(D) Scramjet engine

Q.2 A spring mass-damper system with a mass of 1 kg is found to have a damping ratio of 0.2 and a natural frequency of 5 rad/s. The damping of the system is given by
(A) 2 Ns/m (B) 2 N/s (C) 0.2 kg/s (D) 0.2 N/s

Q.4 An artificial satellite remains in orbit and does not fall to the earth because
(A) the centrifugal force acting on it balances the gravitational attraction
(B) the on-board rocket motor, provide continuous boost to keep it in orbit
(C) its transverse velocity keeps it from hitting the earth although it falls continucusly
(D) due to its high speed it derives sufficient lift from the rarefied atmosphere

Q.7 For maximum range of a glider, which of the following conditions is true?
(A) lift to drag ratio is maximum
(B) rate of descent is minimum
(C) descent angle is maximw
(D) lift to weight ratio is maximum

Q.8 An airplane with a larger wing as compared to a smaller wing will necessarily have
(A) more longitudinal static stability
(B) less longitudinal static stability
(C) same longitudinal static stability
CD) more longitudinal static stability for an aft tail airplane if aerodynamic center of the larger wing is behind the center of gravity of the airplane

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