Revised scheme for B.Tech. - Punjab Technical University
Revised scheme for B.Tech. - Punjab Technical University
Revised scheme for B.Tech. - Punjab Technical University
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PTU/BOS/ME/101/10-06-2005/BATCH-2003<br />
DE/ME-1.9 GAS DYNAMICS<br />
Internal Marks: 40 L T P<br />
External Marks: 60 3 1 0<br />
Total Marks: 100<br />
1. Basic concepts of Gas Dynamics and Gas Properties:<br />
Definition: Units and dimensions. The concepts of continuous, properties of the<br />
continuum. Methods of describing fluid motion, Lagrangian method. Eulerian Method.<br />
The integral <strong>for</strong>m of the equations of Conservations of Mass. Momentum and energy<br />
as applied to Control Volumes, applications to the study flow of inviscid compressible<br />
fluids.<br />
b) Fundamentals Equations Study of One Dimensional Flow :<br />
Continuity equation, the momentum equation, the dynamic equation and Euller’s<br />
equation. Bernoulli’s equation, thrust function, steady flow energy equation.<br />
c) Isentropic Flow:<br />
Introduction, Acoustic velocity, Mach number, Mach line and Mach angle.<br />
Classification of flows, Karman’s rules supersonic flow, flow parameters, Critical<br />
conditions stagnation values.<br />
d) Flow in Ducts with Heating or Cooling:<br />
Stagnation temp. change, governing equations, Rayleigh lines, choking effects in<br />
simple to change. Maximum heat transfer.<br />
e) Flow in constant- Area Ducts with friction:<br />
Friction loss, the friction parameter, Fannolines, effect of the increase of inlet Mach<br />
number and duct length. Chocking due to friction.<br />
Isothermal flow through long ducts.<br />
f) Normal Shock Waves:<br />
Formation of shock waves, weak waves, compression waves. Governing relations of<br />
the Normal shock, Pressure. Temperature, Density, Mach number across shock.<br />
g) Oblique shocks: Oblique shock equations, shock geometry, shock polars.<br />
h) Flow through Nozzles:<br />
The Converging diverging nozzle, area ratio <strong>for</strong> complete expansion, effect of varying<br />
back pressure on nozzle flow. Under-expansion and over-expansion in nozzle flow.<br />
Losses in nozzle.<br />
i) Flow through Diffusers:<br />
Classification of diffusers, internal compression subsonic diffuser, velocity gradient,<br />
effect of friction and area change, the conical internal-compression subsonic diffuser,<br />
external compression subsonic diffuser, supersonic diffuser, normal shock<br />
supersonic diffuser, the converging diverging supersonic diffuser.<br />
j) Introduction to Multidimensional Flow:<br />
The equation of continuity, the momentum equations, Bernoulli,s equation, the<br />
energy equation, Navier-Stock’ Equations, Potential Flow.<br />
Books<br />
i. Thermodynamics of Compressible Fluid flow by Shaprio.<br />
ii. Computational Gas Dynamics by Culbert B. Laney, Cambridge<br />
<strong>University</strong> Press