FLOW AROUND A CORNER FOR AIR IN EQUILIBRIUM (PRANDTL-MEYER EXPANSION)

The document contains a theoretical treatment of the supersonic flow of air around a corner, using the assumptions made by Prandtl and develped by Meyer.

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Bibliographic Details
Main Author: D'Attorre,L
Format: Report
Language:English
Subjects:
AIR
COMPUTER PROGRAMMING
DEFLECTION
DENSITY
ENTHALPY
EQUATIONS OF MOTION
EQUATIONS OF STATE
EQUILIBRIUM(PHYSIOLOGY)
FLOW
Fluid Mechanics
MATHEMATICAL ANALYSIS
PRANDTL-MEYER EXPANSION
PRESSURE
STREAM FUNCTIONS
SUPERSONIC CHARACTERISTICS
TEMPERATURE
TWO DIMENSIONAL FLOW
WALLS
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Description
Summary:The document contains a theoretical treatment of the supersonic flow of air around a corner, using the assumptions made by Prandtl and develped by Meyer.