Roll No. [T T TTT T[] [ ] Total No. of Pages : 03
Total No. of Questions : 09
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B.Tech.(Aerospace Engg.) (2012 Onwards) (Sem.-6)
COMPUTATIONAL FLUID DYNAMICS
Subject Code : ASPE-309
M.Code : 72454
Time : 3 Hrs. Max. Marks : 60
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INSTRUCTIONS TO CANDIDATES :
- SECTION-A is COMPULSORY consisting of TEN questions carrying TWO marks each.
- SECTION-B contains FIVE questions carrying FIVE marks each and students have to attempt any FOUR questions.
- SECTION-C contains THREE questions carrying TEN marks each and students have to attempt any TWO questions.
SECTION-A
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Q1 Answer briefly :
- Parallel computing
- Finite element method.
- Serial Computing
- Viscous flow
- Flux variables
- Time accurate-solution
- Stretched Grid
- Boundary fitted Grid
- Explicit solution
- Contour plot
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SECTION-B
Q2 Explain the physical significance of various terms in the Euler’s equation (Momentum Equation) given below :
?(?u)/?t +?.(?uV)= -?p/?x + fx
?(?v)/?t +?.(?vV)= -?p/?y + fy
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?(?w)/?t +?.(?wV)= -?p/?z + fzQ3 Show that the Laplace’s equation given below is an elliptic equation :
?2/?x2 + ?2/?y2 = 0
Q4 Explain two of the computer graphic techniques used in cfd.
Q5 Explain Crank-Nicolson’s method for Implicit solution techniques.
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Q6 The generic form of the system of governing equations is given below. Explain space marching and time marching for the solution of these equations.
?U/?t + ?F/?x + ?G/?y + ?H/?z = 0
SECTION-C
Q7 One dimensional heat conduction equation with constant thermal diffusivity is given below :
?T/?t = a ?2T/?x2
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Obtain difference equation and explain explicit time marching approach for solution of the one dimensional heat conduction equation.
Q8 The Lax-Wendroff technique is explicit, finite-difference method particularly suited to marching solutions. Consider the Euler’s Equation.
?/?t + u ?/?x + v ?/?y + ? ?u/?x + ? ?v/?y = 0
?u/?t + u ?u/?x + v ?u/?y + (1/?) ?p/?x = 0
?v/?t + u ?v/?x + v ?v/?y + (1/?) ?p/?y = 0
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Set up a numerical solution of Euler’s equation using Lax-Wendroff Technique.
Q9 Write short notes on the following :
- Eigen value method for classifications of governing partial differential equations.
- General transformation of the governing equations from physical space to computational space.
NOTE : Disclosure of Identity by writing Mobile No. or Making of passing request on any page of Answer Sheet will lead to UMC against the Student.
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This download link is referred from the post: PTU B.Tech Question Papers 2020 March (All Branches)
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