Pressure distribution across the shock layer for M ∞ = 21, Re L = 6 .

Pressure distribution across the shock layer for M ∞ = 21, Re L = 6 .

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Aero Fundamentals #23] Pressure Distribution Over An Airfoil

Aero Fundamentals #23] Pressure Distribution Over An Airfoil

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Pressure distribution across the shock layer for M ∞ = 21, Re L

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Pressure distribution across the shock layer for M ∞ = 21, Re L

Aero Fundamentals #23] Pressure Distribution Over An Airfoil