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Concept
Normal Shock Relations
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Summary
Normal Shock Relations
describe the
Abrupt changes in flow properties
such as pressure, temperature, and density that occur when a
Supersonic Flow
encounters a
Shock Wave
perpendicular to the
Flow Direction
. These relations are crucial for understanding and predicting the behavior of
High-speed aerodynamic systems
and are derived from the
Conservation Laws
of mass, momentum, and energy across the
Shock Wave
.
Concepts
Supersonic Flow
Shock Wave
Conservation Of Mass
Conservation Of Momentum
Conservation Of Energy
Mach Number
Pressure Ratio
Temperature Ratio
Density Ratio
Entropy Change
High-Speed Flow
Relevant Degrees
Aerodynamics 70%
Dynamics 20%
Liquid Motion 10%
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