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Jackson, Charlie M.
ID:
1395048
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Jackson, Charlie M.
Jackson Charlie M.
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A method for calculating the aerodynamic loading on wing-body combinations at small angles of attack in supersonic flow
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A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow
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A method for determining the total drag of a pointed body of revolution in supersonic flow with turbulent boundary layer
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