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The calculation of wave drag of a family of low-drag axi-symmetric nose shapes of fineness ratio 4.5 at zero incidence at supersonic speeds
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The calculation of wave drag of a family of low-drag axi-symmetric nose shapes of fineness ratio 4.5 at zero incidence at supersonic speeds

College of Aeronautics

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The calculation of wave drag of a family of low-drag axi-symmetric nose shapes of fineness ratio 4.5 at zero incidence at supersonic speeds by College of Aeronautics. Published by Cranfield College of Aeronautics in 1954. Publication and catalogue information, links to buy online and reader comments.

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