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Book
Airfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range
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Authors:
Chapman, Dean R.
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United States.
Year: 1952 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,
Year: 1952 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,
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Keywords
Aerodynamic load. --- Aerodynamics, Supersonic. --- Aerofoils. --- Drag (Aerodynamics)
Book
Die Ernährung : Physiologie - Pathologie - Therapie
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