#1
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Sir I am searching for the GATE Question Papers with Solutions so please can you give me the papers and tell me from where can I download the papers and provide me the link that can give me the free download of the papers?
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#8
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please mail me 2000-2011 previous papers with solutions mail id mail.vijayavani@gmail.com |
#10
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As you are looking for Aerospace Engineering question paper of GATE exam , here i am providing list of few questions for your idea. Q. 1Which 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 Q.2The critical Mach number for a flat plate of zero thickness, at zero angle of attack, is _________ Q.3A damped single degree-of-freedom system is vibrating under a harmonic excitation with an amplitude ratio of 2.5 at resonance. The damping ratio of the system is Q.4 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 Q.5 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 Q6 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 Q.7 Which one of the following statements is NOT TRUE for a supersonic flow? (A) Over a gradual expansion, entropy remains constant (B) Over a sharp expansion corner, entropy can increase (C) Over a gradual compression, entropy can remain constant (D) Over a sharp compression corner, entropy increases ![]() ![]() ![]() ![]() ![]() ![]() ![]() ![]() ![]() ![]() For more questions , here i am giving attachment
__________________ Answered By StudyChaCha Member |