GATE AE 2020 Paper 1 — page 13

Complete GATE AE 2020 Paper 1 overview, original pages and practice · Timed previous-paper practice

Questions 37–39 of 65. Imported answers require review unless explicitly marked reviewed.

Paper practice 65 questionsPage 13 of 22

A wedge shaped airfoil is placed in a supersonic flow as shown in the figure (not to scale). The corners of the wedge are at

, respectively. Which one of the following represents the correct static pressure profiles along

and

Diagram for Aerospace Engineering question 27

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Diagram for Aerospace Engineering question 27 (figure 2)

Diagram for Aerospace Engineering question 27 (figure 3)

Diagram for Aerospace Engineering question 27 (figure 4)

Diagram for Aerospace Engineering question 27 (figure 5)

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The value of Poisson’s ratio at which the shear modulus of an isotropic material is equal to the bulk modulus is

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A load

is applied to the free end of a stepped cantilever beam as shown in the figure. The Young’s modulus of the material is

, and the moments of inertia of the two sections of length 2 m and 1 m are

and

, respectively. Ignoring transverse shear and stress concentration effects, the deflection at the point where the load is applied at the free end of the cantilever is

Diagram for Aerospace Engineering question 29

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2020 · Paper 1

Question 27

Question 28

Question 29