Semester : SEMESTER 7
Subject : Computational Fluid Dynamics
Year : 2020
Term : DECEMBER
Branch : AERONAUTICAL ENGINEERING
Scheme : 2015 Full Time
Course Code : AO 401
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۸ 00000A.0401121901 Pages: 2
Reg No.: Name:
APJ ABDUL KALAM TECHNOLOGICAL UNIVERSITY
Seventh Semester B.Tech Degree Examinations (Regular and Supplementary), December 2020
Course Code: AO401
Course Name: COMPUTATIONAL FLUID DYNAMICS
Max. Marks: 100 Duration: 3 Hours
PART A
Answer any three full questions, each carries 10 marks. Marks
1 Derive an expression for momentum equation in conservation form expressing (10)
in terms of both body and surface forces?
2 Describe in detail about source panel method for numerical solution of non- (10)
lifting flow over arbitrary bodies and hence derive an expression for coefficient
of pressure over an aerofoil.
3 Classify the following system of PDE’s (10)
du av
—+—=0
0 dy
ov du
Ox 909
where, u and v are the two dependent variables
4 9) Whatis grid generation? (2)
b) Strong conservative form of a _ governing flow equations 15 (8)
ಎ ಜ್ =J. For this unsteady flow in two special dimensions
with no source term. Transform this into computational plane.
PART B
Answer any three full questions, each carries 10 marks.
5 Discuss about the effect of numerical dissipation and dispersion by deriving the (10)
modified form of 1-1) wave equation.
6 Discuss the consistency of 1-D linear conduction equation (10)
eu au
ہے جح سے ہے
0६2 Ox?
7 Using Von Neumann Stability Analysis, obtain the criterion for stability of (10)
Explicit method of 1D heat equation by using FTCS scheme.
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