Approximate formulae for the lift and drag of wedge aerofoil sections at high supersonic speeds
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Approximate formulae for the lift and drag of wedge aerofoil sections at high supersonic speeds
L. C. Squire
URI:
https://reports.aerade.cranfield.ac.uk/handle/1826.2/877
Date:
1966
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Aeronautical Research Council Current Papers
[1393]
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