GATE 2019-20 Aerospace Engineering Question Papers Answers

GATE 2019-20 Aerospace Engineering Question Papers Answers.

GATE i.e. Graduate Aptitude Test in Engineering Aerospace Engineering 2019-20 Exam Has been Conducted by IISc Bangalore IIT Bombay IIT Delhi IIT Guwahati IIT Kanpur IIT Kharagpur IIT Madras IIT Roorkee. This GATE AE 2019-20 examination is the procedure to get the admission in M.Tech

GATE Aerospace Engineering i.e. AE Question Paper, This GATE AE 2019-20 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 2019-20 question paper in pdf file for GATE AE you can download it in FRAE, if GATE Aerospace Engineering 2019-20 paper in text for GATE AE you can download GATE AE 2019-20 page also just Go to menu bar, Click on File->then Save.

GATE 2019-20 Aerospace Engineering Question Papers Answers

GATE AE 2019-20 Question paper Free Download PDF is available in www.oldquestionpapers.net which has been provided by many students this GATE Aerospace Engineering 2019-20 paper is available for all the students in FREE and also GATE AE 2019-20 question paper fully solved i.e with answer keys and solution.

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At 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

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