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What is Oblique Shock and Expansion Waves Module about?

This document is a learning module on oblique shock waves and expansion fans from the Philippine State College of Aeronautics. It contains information on: - Oblique shock waves that occur when supersonic flow is turned into itself, causing a pressure increase. Expansion fans occur when flow is turned away, decreasing pressure. - Equations that govern oblique shock waves involving changes in velocity, pressure, density across the shock. - How to calculate the normal and tangential components of velocity

Author

JamilaWeinPerilloQuintana

Language

EN