Aerospace Engineering Gate Yearwise
Aerospace Gate 2025
Aerospace Gate 2024
Aerospace Gate 2023
Aerospace Gate 2022
Aerospace Gate 2021
Aerospace Gate 2020
Aerospace Gate 2019
Aerospace Gate 2018
Aerospace Gate 2017
Aerospace Gate 2016
Aerospace Gate 2015
Aerospace Gate 2014
Aerospace Gate 2013
Aerospace Gate 2012
Aerospace Gate 2011
Aerospace Gate 2010
Aerospace Gate 2009
Aerospace Gate 2024
Aerospace Gate 2023
Aerospace Gate 2022
Aerospace Gate 2021
Aerospace Gate 2020
Aerospace Gate 2019
Aerospace Gate 2018
Aerospace Gate 2017
Aerospace Gate 2016
Aerospace Gate 2015
Aerospace Gate 2014
Aerospace Gate 2013
Aerospace Gate 2012
Aerospace Gate 2011
Aerospace Gate 2010
Aerospace Gate 2009
Aerospace Engineering GATE 2025 Questions with Answer
Ques 53 Structures
A uniform symmetric cross-section cantilever beam of length L is subjected to a transverse force P at the free end, as shown in the figure. The Young's modulus of the material is E and the moment of inertia is I. Ignoring the contributions due to transverse shear, the strain energy stored in the beam is

Ques 54 Structures
In the given figure, plate ABCD in its undeformed configuration (solid line) is a rhombus with all the internal angles being 90°. The lengths of the undeformed diagonals are 20 cm. ABCD deforms as shown by the dotted lines. Upon deformation, diagonal AC reduces to 19.96 cm and BD increases to 20.04 cm. In the given x-y coordinate system, the engineering shear strain γxy is equal to


Total Unique Visitors
Loading......