GATE AE Question Paper 2010 Aerospace Engineering

GATE AE Question Paper 2010 Aerospace EngineeringGATE AE Question Paper 2010 Aerospace Engineering.

GATE i.e. Graduate Aptitude Test in Engineering Aerospace Engineering 2010 Exam Has been Conducted by IISc Bangalore IIT Bombay IIT Delhi IIT Guwahati IIT Kanpur IIT Kharagpur IIT Madras IIT Roorkee. This GATE AE 2010 examination is the procedure to get the admission in M.Tech

GATE Aerospace Engineering i.e. AE Question Paper, This GATE AE 2010 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 2010 question paper in pdf file for GATE AE you can download it in FRAE, if GATE Aerospace Engineering 2010 paper in text for GATE AE you can download GATE AE 2010 page also just Go to menu bar, Click on File->then Save.

GATE AE Question Paper 2010 Aerospace Engineering

GATE AE 2010 Question paper Free Download PDF is available in which has been provided by many students this GATE Aerospace Engineering 2010 paper is available for all the students in FRAE and also GATE AE 2010 question paper fully solved i.e with answer keys and solution.

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Q.3 An aircraft is climbing at a Consan speed in a traigiu line at 3 steep angle of climb. The load
factor h suslairis dunog the climb is:
(A) equal to I O (B) greater than I 0
(C) positive but less than 1.0 (D) dependant on the weight of the aircraft

Q.4 In a generai ca. of a homogeneous material under (benno-mechanicai loading the number 01
distinct components of the state of stress is
(A)3 (8)4 (C)5 (D)6

Q.6 All other factors remaining constant, lithe weight of an awcraft increases by 30% then the takeoff
dIstance increases by approximtely:
(A) 15% (B) 30% (C) 70% (D) 105%

Q.7 A vertical slender rod is suspended by i hingc at the (op and hangs freely. It is heated until it attains
a uniform temperature, 7’. Neglecting the effect of graviy, the rod has
(A) Stress but rio strain (B) Siraui but no stress
(C) Both stress and strain (D) Neither Stress nor strain

Q.8 An aircraft stalls at a speed Df 40 rn/s in straight and Iciel flighi. The slowest speed at which this
aircraft can eecute a level um at a bank angle of 60 degrees is;
(A) 28.3 ni/s (13)400 in/s (C) 56.6 mIs (Cl) O.o rn/s

Q.9 The cigea-values of a real symmetric matri* are always
(A) positive (B) imaginary
(C) real (0) compkx conjugate pairs

Q. 12 The absolute ceiling of an aircraft is the alLilude above which l:
(A) can never reach
(B) cannot sustain level flight at a constant speed
(C) can pcrform accelerated fligh as well as straight and level flight at a con slant speed
(D) can perform straight and level flight at a constant speed only

Q.15 The angular momentum, about the centre of mass of the earTh. olan artificial satellite in a highly
ellipLical orbit is
(A) a maximum when ihe satellite is farthest from the earth
(B) a constant
(C) proportional w thy speed of the satellite
(I)) proportional to the square of the speed of the sitcllite


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