GATE AE 2026 • Q40
MCQ • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Consider a unit square body as shown in the figure below. The body is subjected to the deformation field u = -ay and v = ax, where 'a' is a constant. Due to the application of this deformation field, the body undergoes _______ in the x-y plane.
Official Key: D ➔
GATE AE 2026 • Q57
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
WA and WB are the respective maximum take-off weights of an aircraft for two ambient air conditions given below. Condition A: p = 1 bar, T = 50 oC; Condition B: p = 0.66 bar, T = -30 oC If all other parameters relevant for take-off are kept the same in these two conditions, the ratio WB/WA is ________ (rounded off to 3 decimal places).
Official Key: 0.875 ➔
GATE AE 2026 • Q60
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
A stepped cantilever beam, made of a material having Young's modulus E = 200 GPa, is shown in the figure below. The length and the moment of inertia of the beam from point A to B are L1 = 100 mm and I1 = 100 mm4, respectively. The length and the moment of inertia of the beam from point B to C are L^2 = 100 mm and I^2 = 700 mm4, respectively. A shear force P = 30 N is applied at point A of the beam. The magnitude of the deflection of the beam at point A is ________ mm (rounded off to 1 decimal place).
Official Key: 1.0 ➔
GATE AE 2025 • Q28
MCQ • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
A stress field is given by $\sigma_{xx} = \sigma_{zz} = C_1y$; $\sigma_{yy} = C_2y$; $\tau_{xy} = \tau_{yz} = \tau_{zx} = 0$, where $C_1$ and $C_2$ are non-zero constants. If the stress field satisfies equilibrium, which one of the following options is correct?
Official Key: B ➔
GATE AE 2025 • Q29
MCQ • 1M
Subtopic: Euler Buckling of Columns & Energy Methods
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:
Official Key: A ➔
GATE AE 2025 • Q30
MCQ • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
In the given figure, plate ABCD in its undeformed configuration (solid line) is a rhombus with all the internal angles being 90o. 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 $\gamma$xy is equal to ____.
Official Key: A ➔
GATE AE 2025 • Q37
MCQ • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
A 1 m long rod is to be designed to support an axial tensile load P (P >> weight of the rod). The material for the rod is to be chosen from one of the four provided in the table. Using strength-based failure criterion for design, which material results in the lowest weight of the rod? Properties Material Material Material Material Density (kg/m^3) 2700 4500 7800 9000 Young's modulus (GPa) 70 115 200 130 Yield Strength (MPa) 270 900 520 540
Official Key: B ➔
GATE AE 2025 • Q58
NAT • 2M
Subtopic: Euler Buckling of Columns & Energy Methods
A prismatic vertical column of cross-section a × 0.5a and length l is rigidly fixed at the bottom and free at the top. A compressive force P is applied along the centroidal axis at the top surface. The Young's modulus of the material is 200 GPa and the uniaxial yield stress is 400 MPa. If the critical value of P for yielding and for buckling of the column are equal, the value of ( l a) is _____(rounded off to one decimal place).
Official Key: 5.05 ➔
GATE AE 2024 • Q52
NAT • 2M
Subtopic: Mohr's Circle for Plane Stress
The state of stress at a point is caused by two separate loading cases. One of them produces a pure uniaxial tension along the x′ direction, and other one produces a pure uniaxial compression along the y′ direction, as shown in the figure. The sum of maximum and minimum principal stresses for the resultant state of stress caused by both loads acting simultaneously is ___________ N/mm 2 (rounded off to 1 decimal place).
Official Key: 0.0 ➔
GATE AE 2024 • Q56
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Consider the plane strain field given by 𝜀xx = 10 xy2, 𝜀yy = -5 x2y and $\gamma$xy = A xy (2x - y) where, A is a constant and $\gamma$xy is the engineering shear strain . The value of the constant A for the strain field to be compatible is _____________ (rounded off to 1 decimal place).
Official Key: 5.0 ➔
GATE AE 2023 • Q23
MCQ • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Consider the four basic symmetrical flight loading conditions corresponding to the corners of a typical V-n diagram. For one of these flight loading conditions, it is observed that (i) the compressive bending stresses have a maximum value in the bottom aft region (see figure) of the wing cross-section; and (ii) the tensile bending stresses are maximum in the upper forward region (see figure) of the wing cross-section. For the preceding observations, select the corresponding flight loading condition from the options given.
Official Key: D ➔
GATE AE 2023 • Q40
MCQ • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Consider a general aviation airplane with weight 10 kN and a wing planform area of 15 m^2. The drag coefficient of the airplane is given as 0 2 D D LC C KC=+ with 0 0.025DC = and 0.05K = . For level flight at an altitude where the density is 0.60 kg/m3 and thrust 1 kN, the maximum cruise speed is (rounded off to the nearest integer)
Official Key: A ➔
GATE AE 2023 • Q42
MSQ • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Consider the equation sindy ay xdx += , where a and $\omega$ are constants. Given 1 at 0yx== , select all correct statement(s) from the following as x → .
Official Key: C, D ➔
GATE AE 2023 • Q48
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
The thickness of a uniform hollow circular shaft is equal to the difference between the outer radius and the inner radius. The ratio of the inner diameter to outer diameter of the shaft is 0.5 . For the shaft reacting to an applied torque, the ratio of the maximum shear stress to the maximum shear stress thin wall - obtained using the thin-wall approximation is . (round off to one decimal place)
Official Key: 1.2 ➔
GATE AE 2023 • Q49
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
A rigid bar AB is subjected to a uniformly distributed load of 100 N/m as shown in the figure. The bar is supported by rod CD, with A, C, and D as pin joints. The rod CD has axial stiffness of 40 N/mm. The vertical deflection at point D is __________ mm. (round off to nearest integer)
Official Key: 10.0 ➔
GATE AE 2023 • Q50
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
A cantilever beam of length 2a is loaded at the tip with force F as shown in the figure. The beam is supported in the middle by a roller with a pin. The magnitude of moment reaction at the built -in end of the beam is Fa, where is ______ . (round off to one decimal place)
Official Key: 0.5 ➔
GATE AE 2022 • Q16
MCQ • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Consider steady, two-dimensional, incompressible flow over a non-porous flat plate as shown in the figure. For the control volume $PQRS$, the speed, $u_\infty$, at section $PQ$ is uniform and the speed at section $RS$ is given by $u(y) = A_0 \left(\frac{y}{h}\right)^n$, where $n$ is a positive integer. The value of $A_0$ for which the flow through section $PS$ will vanish is:
Official Key: B ➔
GATE AE 2022 • Q20
MCQ • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
A beam with a symmetrical T-shaped cross-section, as shown in the figure, is subjected to pure bending. The maximum magnitude of the normal stress is realised:
Official Key: B ➔
GATE AE 2022 • Q24
MSQ • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
If $\hat{a}, \hat{b}, \hat{c}$ are three mutually perpendicular unit vectors, then $\hat{a} \cdot (\hat{b} \times \hat{c})$ can take the value(s):
Official Key: B, C ➔
GATE AE 2022 • Q28
MSQ • 1M
Subtopic: Mohr's Circle for Plane Stress
Let $\sigma$ and $\tau$ represent the normal stress and shear stress on a plane, respectively. The Mohr circle(s) that may possibly represent the state of stress at points in a beam of rectangular cross-section under pure bending is/are:
Official Key: B, C ➔
GATE AE 2022 • Q31
NAT • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
The arc length of the parametric curve: x = cos $\theta$ , y = sin $\theta$ , z = $\theta$ from $\theta$ = 0 to $\theta$ = 2$\pi$ is equal to ________ (round off to one decimal place).
Official Key: 8.85 ➔
GATE AE 2022 • Q33
NAT • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
The two-dimensional plane-stress state at a point is: $\sigma_{xx} = 110\text{ MPa}; \sigma_{yy} = 30\text{ MPa}; \tau_{xy} = 40\text{ MPa}$. The normal stress, $\sigma_n$, on a plane inclined $45^\circ$ as shown in the figure is ______ $\text{MPa}$ (round off to the nearest integer).
Official Key: 110.0 ➔
GATE AE 2022 • Q41
MCQ • 2M
Subtopic: Airframe Structural Analysis & Trusses
A horizontal load $F$ is applied at point $R$ on a two-member truss, as shown in the figure. Both the members are prismatic with cross-sectional area, $A_0$, and made of the same material with Young's modulus $E$. The horizontal displacement of point $R$ is:
Official Key: C ➔
GATE AE 2022 • Q45
MSQ • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
For a conventional airplane in straight, level, constant velocity flight condition, which of the following condition(s) is/are possible on Euler angles $(\phi, \theta, \psi)$, angle of attack $(\alpha)$ and the sideslip angle $(\beta)$?
Official Key: A ➔
GATE AE 2022 • Q50
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
A rotational velocity field in an air flow is given as ˆ ˆV ayi bxj , with a = 10 s-1, b = 20 s-1. The air density is 1.0 kg/m3 and the pressure at (x, y) = (0 m, 0 m) is 100 kPa. Neglecting gravity, the pressure at (x, y) = (6 m, 8 m) is _____ kPa (rounded off to nearest integer).
Official Key: 89.5 ➔
GATE AE 2022 • Q57
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Given: The tip deflection and tip slope for a tip loaded cantilever of length $L$ are $\frac{NL^3}{3EI}$ and $\frac{NL^2}{2EI}$, respectively, where $N$ is the tip force and $EI$ is the flexural rigidity. A cantilever $PQ$ of rectangular cross-section is subjected to transverse load, $F$, at its mid-point. Two cases are considered as shown in the figure. In Case I, the end $Q$ is free and in Case II, $Q$ is simply supported. The ratio of the magnitude of the maximum bending stress at $P$ in Case I to that in Case II is ______ (rounded off to one decimal place).
Official Key: 2.65 ➔
GATE AE 2022 • Q58
NAT • 2M
Subtopic: Euler Buckling of Columns & Energy Methods
A simply supported Aluminium column of length 1 m and rectangular cross- section w × t with t ≤ w, is subjected to axial compressive loading. Young's modulus is 70 GPa. Yield stress under uniaxial compression is 120 MPa. The value of t at which the failure load for yielding and buckling coincide is _______mm.
Official Key: 45.5 ➔
GATE AE 2022 • Q60
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
A $10\text{ kN}$ axial load is applied eccentrically on a rod of square cross-section ($1\text{ cm} \times 1\text{ cm}$) as shown in the figure. The strains measured by the two strain gages attached to the top and bottom surfaces at a distance of $0.5\text{ m}$ from the tip are $\epsilon_1 = 0.0016$ and $\epsilon_2 = 0.0004$, respectively. The eccentricity in loading, $e$, is ______ $\text{mm}$.
Official Key: 1.0 ➔
GATE AE 2021 • Q49
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Q.49 A rigid horizontal bar ABC, with roller support at A, is pinned to the columns BD and CE at points B and C, respectively as shown in figure. The other end of the column BD is fixed at D, whereas the column CE is pinned at E. A vertical load P is applied on the bar at a distance 'a' from
Official Key: 0.42 ➔
GATE AE 2021 • Q50
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Q.50 A two-cell wing box is shown in the figure. The cell walls are 1.5 mm thick and the shear modulus G = 27 GPa. If the structure is subjected to a torque of 12 kNm, then the wall AD will experience a shear stress of magnitude
Official Key: 98.25 ➔
GATE AE 2021 • Q52
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Q.52 A 3 m x 1 m signboard is supported by a vertical hollow pole that is fixed to the ground. The pole has a square cross section with outer dimension 250 mm. The yield strength of the pole material is 240 MiPa. To sustain a wind pressure of 7.5 kPa, the dimension d of the pole is _
Official Key: 5.0 ➔
GATE AE 2020 • Q15
MCQ • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Given access to the complete body geometry, surface static pressure distribution, and wall shear stress distribution over a body placed in a uniform flow, one can compute:
Official Key: D ➔
GATE AE 2020 • Q52
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
The two masses of the two degree of freedom system shown in the figure are given initial displacements of 2 cm (xz) and 1.24 cm (x^2). The system starts to vibrate in the first mode. The first mode shape of this system is d = [1 a]', where a = . (round off to two decimal places). 1x, (t) 1x3(t)
Official Key: 3.565 ➔
GATE AE 2020 • Q53
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
As shown in the figure, a beam of length 1 m is rigidly clamped at one end ($x = 0$) and simply supported at the other ($x = 1$ m). Under the action of a uniformly distributed downward load of $w = 10$ N/m, the magnitude of the vertical reaction force (in N) at the simply supported end is _________ (round off to two decimal places).
Official Key: 3.75 ➔
GATE AE 2019 • Q34
NAT • 1M
Subtopic: Mohr's Circle for Plane Stress
For the state of stress shown in the figure, the normal stress, $\sigma_n$, on a plane inclined at 45 degrees to the principal planes with $\sigma_1 = 300$ MPa and $\sigma_2 = 200$ MPa is _________ MPa (round off to the nearest integer).
Official Key: 250.0 ➔
GATE AE 2019 • Q60
NAT • 2M
Subtopic: Euler Buckling of Columns & Energy Methods
All the bars in the given truss are elastic with Young's modulus 200 GPa, and have identical cross-sections with moment of inertia $I = 0.1$ cm$^4$. The lowest value of the load $P$ (in kN) at which the truss fails due to buckling of member BC (length $L = 10$ cm) is _________ kN (round off to the nearest integer).
Official Key: 560.0 ➔
GATE AE 2019 • Q61
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
A solid circular shaft is designed to transmit a torque $T$ with a factor of safety of 2. It is proposed to replace the solid shaft by a hollow shaft of the same material and identical outer radius. If the inner radius is half the outer radius, the factor of safety for the hollow shaft is _________ (round off to 1 decimal place).
Official Key: 1.85 ➔
GATE AE 2019 • Q62
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
In the structure shown in the figure, bars AB and BC are made of identical material and have circular cross-sections of 10 mm radii. The yield stress of the material under uniaxial tension is 280 MPa. Using the von Mises yield criterion, the maximum load (in N) along the z-direction (perpendicular to the plane of paper) that can be applied at C, such that AB does not yield is _________ N (round off to the nearest integer). (Take $AB = 0.55$ m, $BC = 0.50$ m)
Official Key: 315.0 ➔
GATE AE 2018 • Q17
MCQ • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Determine the correctness or otherwise of the following statements, [a] and [r]: [a] A closed-section box beam configuration is used in aircraft wings. [r] Closed-section box beam configuration is capable of resisting torsional loads.
Official Key: A ➔
GATE AE 2018 • Q31
NAT • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Which of the following statement(s) is/are true about the state of a body in plane strain condition? P: All the points in the body undergo displacements in one plane only, for example the x -y plane, leading to 𝜀zz = $\gamma$xz = $\gamma$yz = 0. Q: All the components of stress perpendicular to the plane of deformation, for example the x-y plane, of the body are equal to zero, i.e. $\sigma$zz = $\tau$xz = $\tau$yz = 0. R: Except the normal component, all the other components of stress perpendicular to the plane of deformation of the body, for example the x -y plane, are equal to zero, i.e. $\sigma$zz ≠ 0, $\tau$xz = $\tau$yz = 0.
Official Key: 1185.75 ➔
GATE AE 2018 • Q52
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
The components of stress in a bo dy under plane stress condition, in the absence of body forces, is given by: $\sigma$xx = Ax2; $\sigma$yy = 12x2 - 6y2 and $\sigma$xy = 12xy. The coefficient, A, such that the body is under equilibrium is _____ (accurate to one decimal place).
Official Key: 210.0 ➔
GATE AE 2018 • Q62
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
The components of stress in a body under plane stress condition, in the absence of body forces, is given by: $\sigma_{xx} = Ax^2; \sigma_{yy} = 12x^2 - 6y^2$ and $\sigma_{xy} = 12xy$. The coefficient, $A$, such that the body is in static equilibrium is _________.
Official Key: -6.0 ➔
GATE AE 2017 • Q31
NAT • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Correct: 2 Wrong: -0.66 "If you are looking for a history of India, or for an account of the rise and fall of the British Raj. or for the reason of the cleaving of the subcontinent into two mutually antagonistic parts and the effects this mutilation will have in the respective sections. and ultimately on Asia, you will not find it in these pages; for though I have spent a lifetime in the country, I lived too near the seat of events, and was too intimately associated with the actors, to get the perspective needed for the impartial recording of these matters." Which of the following statements best reflects the author's opinion?
Official Key: 0.545 ➔
GATE AE 2017 • Q32
NAT • 1M
Subtopic: Airframe Structural Analysis & Trusses
Each of P. Q. R, S, W. X. Y and Z has been married at most once. X and Y are married and have two children P and Q. Z is the grandfather of the daughter S of P. Further. Z and W are married and are parents of R. Which one of the following must necessarily be FALSE?
Official Key: 0.1665 ➔
GATE AE 2017 • Q51
NAT • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
An aircraft wing is idealized as a cantilever beam of constant width and length $L = 5$ m, carrying a uniformly distributed aerodynamic lift load of $w = 2$ kN/m. If the flexural rigidity of the wing box is $EI = 10^7$ N-m$^2$, the tip deflection (in mm) of the wing is _________ (round off to the nearest integer).
Official Key: 16.0 ➔
GATE AE 2017 • Q52
NAT • 2M
Subtopic: Mohr's Circle for Plane Stress
For the state of plane stress shown in the figure with $\sigma_x = 80$ MPa, $\sigma_y = -20$ MPa, and $\tau_{xy} = 40$ MPa, the minimum principal stress (in MPa) is _________ (round off to the nearest integer).
Official Key: -33.0 ➔
GATE AE 2016 • Q12
NAT • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Determine the correctness or otherwise of the following statements, [a] and [r]: [a]: In a plane stress problem, the shear strains along the thickness direction of a body are zero but the normal strain along the thickness is not zero. [r]: In a plane stress problem, Poisson effect induces the normal strain along the thickness direction of the body.
Official Key: -3.0 ➔
GATE AE 2016 • Q13
MCQ • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Consider four thin -walled beams of different open cross-sections, as shown in the cases (i-iv). A shear force of magnitude 'F' acts vertically downward at the location 'P' in all the beams. In which of the following case, does the shear force induce bending and twisting? Case (i) Case (ii) Case (iii) Case (iv)
Official Key: D ➔
GATE AE 2016 • Q15
MCQ • 1M
Subtopic: Mohr's Circle for Plane Stress
A structural member supports loads, which produce at a particular point, a state of pure shear stress of 50 N/mm 2. At what angles are the principal planes oriented with respect to the plane of pure shear?
Official Key: D ➔
GATE AE 2016 • Q39
MCQ • 2M
Subtopic: Euler Buckling of Columns & Energy Methods
Determine the correctness or otherwise of the following statements, [a] and [r], [a]: Ribs, used in airplane wings, increase the column buckling strength of the longitudinal stiffeners. [r]: Ribs distribute concentrated loads into the structure and redistribute stresses around discontinuities.
Official Key: D ➔
GATE AE 2014 • Q13
MCQ • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Which one of the following objects with inclined face at 45oo , subjected to the given stresses, are in static equilibrium:
Official Key: C ➔
GATE AE 2014 • Q31
NAT • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
For a steady, incompressible two-dimensional flow, represented in Cartesian co-ordinates (xx, yy), a student correctly writes the equation of pathline of any arbitrary particle as, ddxx dddd = aaxx and ddyy dddd = bbyy, wherea and bare constants having unit of (second)-1. If value of a is 5, the value of b is _____. AE 5/11 AE (GATE 2014) - AE
Official Key: 0.5 ➔
GATE AE 2014 • Q40
MCQ • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
A structural member of rectangular cross-section 10mm× 6mm and length 1m is made of steel (Young's modulus is 200GPa and coefficient of thermal expansion is 12 × 10-6 / CCoo ). It is rigidly fixed at both the ends and then subjected to a gradual increase in temperature. Ignoring the three dimensional effects, the structural member will buckle if the temperature is increased by ∆TT CCoo which is
Official Key: B ➔
GATE AE 2014 • Q42
MCQ • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
A cantilevered beam is subjected to a parabolic distribution of shear traction at the right edge while the top and bottom surfaces are traction free. To solve this problem, following Airy's stress function is proposed: $\phi \phi$ = CC1xxyy + CC2xxyy3 + CC3xx2yy2 + CC4xx3yy. This is an admissible Airy's function that would satisfy the bi-harmonic equation as well as the boundary conditions if and only if
Official Key: C ➔
GATE AE 2013 • Q41
NAT • 2M
Subtopic: Euler Buckling of Columns & Energy Methods
In the steel structure (Young's modulus = 200 GPa) shown in the figure, all members have a circular cross-section of radius 10 mm. Column BD is pinned at B and D. The support at A is hinged. The minimum value of load ܲat which the column BD may buckle in Newtons is approximately ____________
Official Key: 1950.0 ➔
GATE AE 2012 • Q32
MCQ • 1M
Subtopic: Airframe Structural Analysis & Trusses
The volume of a solid generated by rotating the region between semi-circle 211y x=- - and straight line y = 1, about x axis, is
Official Key: A ➔
GATE AE 2012 • Q44
MCQ • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
The Airy stress function, 22x xy y$\phi \alpha \beta \gamma$=++ for a thin square panel of size ll× automatically satisfies compatibility. If the panel is subjected to uniform tensile stress, o$\sigma$ on all four edges, the traction boundary conditions are satisfied by
Official Key: A ➔
GATE AE 2012 • Q54
MCQ • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
The internal pressure Yp at yield, based on the von Mises yield criterion, if the vessel is floating in space, is approximately
Official Key: D ➔
GATE AE 2011 • Q26
NAT • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
P L L/2 2011 AEROSPACE ENGINEERING - AE AE Consider a beam in bending with a solid circular cross-section of 1 mm2, which is subjected to a transverse shear force of 1 N. The shear stress at the center of the cross-section (in N/mm2) is
Official Key: 2.5 ➔
GATE AE 2011 • Q27
NAT • 1M
Subtopic: Euler Buckling of Columns & Energy Methods
A simp ly supported slender column of square cross section (width=depth= d) has to be designed such that it buckles at the same instant as it yields. Length of the column is given to be 1.57 m and it is made of a material whose Young's modulus is 200 GPa and yield stress is 240 MPa. The width, d, of the column (in cm) should be
Official Key: 1.325 ➔
GATE AE 2011 • Q36
MCQ • 2M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Which of the following Airy's stress functions could satisfy the given boundary conditions, assuming constant values of xx = P, yy = Q and xy = R, along the boundary? (A) RxyyQxP 2 2 22 (B) RxyxQyP 2 2 22
Official Key: B ➔
GATE AE 2010 • Q21
MCQ • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Following stress state is proposed for a^2-D problem with no body forces: $\sigma$_xx = 3x^2 y + 4y^3, $\sigma$_yy = 5x^2 + 14y^2, $\tau$_xy = -3xy^2 - 7x^2. It satisfies:
Official Key: A ➔
GATE AE 2010 • Q31
MCQ • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
Consider a l-D adiabatic, inviscid, compressible flow of air (R = 287 J/Kg-K, c, = 718 J/Kg-K) through a duct of constant cross-sectional area A=1m'. If the valumetric flow rate is = 680 m/s and stagnation temperature is T, = 580.05 K. then the air temperature inside the duct is
Official Key: B ➔
GATE AE 2008 • Q31
MCQ • 1M
Subtopic: Stress and Strain Tensors & Generalized Hooke's Law
In the definition of the aircraft Euler angles @ (roll), ® (pitch), and v (yaw), the correct sequence of rotations required to make the inertial frame coincide with the aircraft body frame is
Official Key: B ➔
GATE AE 2007 • Q39
MCQ • 2M
Subtopic: Euler Buckling of Columns & Energy Methods
Mises yield criterion or the maximum distortion energy criterion for a plane stress problem with o, and o, as the principal stresses in the plane, and oy as the yield stress, requires
Official Key: C ➔