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May 26, 1959Proceedings of the Royal Society of London A Mathematical and Physical Sciences

A theory of the flow past a slender delta wing with leading edge separation

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Authors

KMK. W. ManglerUniversity of SouthamptonJSJ. H. B. SmithAlbany State University

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Mangler et al. (1959) studied this question.

synapsesocial.com/papers/6a758e7bc96e4a414b5fffddhttps://doi.org/10.1098/rspa.1959.0102
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Also Consider

Synapse has enriched 3 closely related papers on similar clinical questions. Consider them for comparative context:

  1. 1Effect of Leading-Edge Separation on the Lift of a Delta Wing1954 · 209 citations
  2. 2A Superposition Analysis of the Turbulent Boundary Layer in an Adverse Pressure Gradient1951 · 12 citations
  3. 3The Compressible Boundary Layer1952 · 39 citations