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Transonic Panel Method to Determine Loads on Oscillating Airfoils with Shocks - MaRDI portal

Transonic Panel Method to Determine Loads on Oscillating Airfoils with Shocks (Q3904271)

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Transonic Panel Method to Determine Loads on Oscillating Airfoils with Shocks
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    Transonic Panel Method to Determine Loads on Oscillating Airfoils with Shocks (English)
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    1981
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    oscillating airfoils
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    linear lifting surface theories
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    velocity potential panel approach
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    effect of moving shock
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    NACA 64A006 airfoil
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    LTRAN 2 code
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