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- W217163891 abstract "Report presenting a linearized theoretical analysis made to determine minimum-wave-drag airfoil sections for arrow wings having the same airfoil sections at all spanwise sections. Numerical computations of the airfoil shape and wing wave drag were performed for a delta wing and an arrow wing with a ratio of the tangent of the trailing-edge sweep angle to the tangent of the leading-edge sweep angle of 0.4." @default.
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- W217163891 date "1954-05-01" @default.
- W217163891 modified "2023-09-24" @default.
- W217163891 title "Minimum-wave-drag airfoil section for arrow wings" @default.
- W217163891 hasPublicationYear "1954" @default.
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