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JNTU B.Tech III COMPUTATIONAL AERODYNAMICS Previous Question Paper (May - 2019 - R15)

B.Tech | III | II | R15 | May - 2019

Answer PaperPaper Code: 126YWMaximum Marks: 75Time: 3 hours

Note: This question paper contains two parts A and B. Part A is compulsory which carries 25 marks. Answer all questions in Part A. Part B consists of 5 Units. Answer any one full question from each unit. Each question carries 10 marks and may have a, b, c as sub questions.

Part A

125 marks
a

What steps are involved in solving a typical CFD problem?

2 marks

Answer

  1. Pre-processing: Geometry definition, grid generation, and defining boundary conditions.
  2. Solver: Selection of numerical schemes and solving discretized governing equations.
  3. Post-processing: Visualization and analysis of flow field data.
b

Define substantial derivative and explain its physical significance.

3 marks

Answer

The substantial derivative represents the time rate of change of a fluid property following a fluid element moving through the flow field. It is defined as D/Dt = ∂/∂t + (V · ∇). Its physical significance is that it accounts for both the local change at a fixed point and the convective change due to the motion of the fluid particle.

c

What are characteristic lines?

2 marks

Answer

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d

Explain Dirichlet and Neumann boundary conditions for elliptic partial differential equations.

3 marks

Answer

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e

What is Courant number and what is its function?

2 marks

Answer

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f

Differentiate between structured and unstructured grids.

3 marks

Answer

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g

What steps are required in setting up the finite volume method?

2 marks

Answer

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h

List out the differences between finite difference and finite volume methods.

3 marks

Answer

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i

Differentiate between staggered and collocated arrangements of grids in CFD.

2 marks

Answer

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j

Distinguish between SIMPLE and SIMPLER pressure correction algorithms.

3 marks

Answer

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Part B

2

Derive integral forms of continuity equation using flow models of control volume fixed in space and control volume moving with fluid.

10 marks

Answer

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OR
3

Explain shock capturing and shock fitting approaches of handling shocks in CFD with figures. Discuss their relative advantages and disadvantages.

10 marks

Answer

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4

Describe the general method of classifying a system of quasi-linear partial differential equations using Eigen value method.

10 marks

Answer

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OR
510 marks
a

Discuss the concepts of domain of dependence and range of influence for hyperbolic equations using a sketch.

5 marks

Answer

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b

Explain Parabolized Navier-Stokes (PNS) model for viscous flows and discuss its advantages.

5 marks

Answer

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6

Describe explicit and implicit approaches to the numerical solution of fluid flows using sketches and illustrate them for one dimensional heat conduction equation:

[∂T/∂t] = α [∂2T/∂x2]
using finite-difference method.

10 marks

Answer

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OR
7

Describe different types of body-fitted and multi-block grids with the help of sketches.

10 marks

Answer

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8

Discuss cell-centred and cell-vertex approaches of finite volume method with suitable diagrams.

10 marks

Answer

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OR
9

Discuss the general formulation of a numerical scheme based on finite volume method.

10 marks

Answer

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10

Explain MacCormack’s technique for time marching solution of two-dimensional unsteady Euler equations.

10 marks

Answer

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OR
11

Discuss the numerical steps involved in the pressure correction algorithm SIMPLE.

10 marks

Answer

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About this paper

This page contains the question paper of COMPUTATIONAL AERODYNAMICS from JNTU for B.Tech AE III II, May - 2019, R15.

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