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  #1  
Old November 4th, 2012, 06:27 PM
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Default GATE Old Question Papers PDF

Sir I wish to take part in the Graduate Aptitude Test in Engineering and for the better preparation I need the Old Question Papers of the test so please can you give me the question papers and provide me the page where I can get the PDF of the papers?
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  #2  
Old November 5th, 2012, 11:40 AM
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Default Re: GATE Old Question Papers PDF

Graduate Aptitude Test is a well known entrance examination which is provide admission in the various graduate prorgramme.

We are already uploaded the question papers of GATE examination on our website so we are provide you links so you can get the question paper of it easily.

http://studychacha.com/discuss/40937...-download.html

http://studychacha.com/discuss/30512...tions-ece.html
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  #3  
Old March 27th, 2014, 11:53 AM
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Default Re: GATE Old Question Papers PDF

Graduate Aptitude Test for Engineering popularly known as GATE is the national level engineering entrance exam for admission in post graduate engineering courses.

Sample Questions:

At 0 x = 0, the function y = |x| is
(A) continuous but not differentiable
(B) continuous and differentiable
(C) not continuous but differentiable
(D) not continuous and not differentiable

Which one of the following is the most stable configuration of an airplane in roll?
(A) Sweep back, anhedral and low wing
(B) Sweep forward, dihedral and low wing
(C) Sweep forward, anhedral and high wing
(D) Sweep back, dihedral and high wing

Which one of the following flight instruments is used on an aircraft to determine its attitude in flight?
(A) Vertical speed indicator
(B) Altimeter
(C) Artificial Horizon
(D) Turn-bank indicator

A supersonic airplane is expected to fly at both subsonic and supersonic speeds during its whole flight course. Which one of the following statements is TRUE?
(A) Airplane will experience less stability in pitch at supersonic speeds than at subsonic speeds
(B) Airplane will feel no change in pitch stability
(C) Airplane will experience more stability in pitch at supersonic speeds than at subsonic speeds
(D) Pitch stability cannot be inferred from the information given

Which one of the following is favorable for an airplane operation?
(A) Tail wind in cruise and head wind in landing
(B) Tail wind both in cruise and landing
(C) Head wind both in cruise and landing
(D) Head wind in cruise and tail wind in landing

Which one of the following is TRUE with respect to Phugoid mode of an aircraft?
(A) Frequency is directly proportional to flight speed
(B) Frequency is inversely proportional to flight speed
(C) Frequency is directly proportional to the square root of flight speed
(D) Frequency is inversely proportional to the square root of flight speed

Which one of the following is TRUE with respect to Phugoid mode of an aircraft?
(A) Frequency is directly proportional to flight speed
(B) Frequency is inversely proportional to flight speed
(C) Frequency is directly proportional to the square root of flight speed
(D) Frequency is inversely proportional to the square root of flight speed

Here I am attaching the previous year question papers of GATE:








Attached Files
File Type: pdf GATE question papers.pdf (278.5 KB, 12 views)
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