Frictional Flow through Variable Area Ducts

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Presentation transcript:

Frictional Flow through Variable Area Ducts P M V Subbarao Professor Mechanical Engineering Department Better Geometrical Solutions to Convert Macroscopic Kinetic Energy to Microscopic KE & vice Versa…..

Geometry of Isentropic Diffuser/Nozzle

Frictional Adiabatic Flow in A Variable Area Duct Constant Mach number frictional flow

Capacity Loss due to friction Sonic Point : M =1 Velocity at the throat is not sonic and this is the maximum allowable velocity at throat. Sonic velocity occurs in diverging section.

Adiabatic Frictional Flow in A Constant Area Duct tw

Differential Equations for Gas Dynamics of Frictional Flow Through Constant Area Duct

Strange Condition in Adiabatic Frictional Flow through Constant Areas Pipes Critical point at M=1. It is impossible to drive the flow further at M=1. The flow is choked! For subsonic flow dp is negative in the direction of flow. Acceptable. For supersonic flow dp is positve. Strange!

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Gino Girolamo Fanno : Fanno Model : 29 July 1935

Nature of Real Flow in Constant Area Duct Entropy of an irreversible adiabatic system should always increase!

Gino Girolamo Fanno: Fanno Line Adiabatic flow in a constant area with friction is termed as Fanno flow.

M dM dp dT dV <1 +ve -ve >1

Compressible Flow Through Finite Length Duct Integrate over a length l Consider a Mean friction factor over a length l .

Maximum Allowable Length The length of the duct required to give a Mach number of 1 with an initial Mach number Mi Similarly

Compressible Frictional Flow through Constant Area Duct