Supersonic natural laminar flow wing
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United States of America Patent
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Jul 23, 1996
Grant Date -
N/A
app pub date -
Dec 14, 1993
filing date -
Dec 14, 1993
priority date (Note) -
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Abstract
A reverse delta aerodynamic wing has a basic reverse delta wing portion bounded by a leading edge and by a pair of trailing edges extending from respective ends of said leading edge toward a trailing apex point and respective span-wise wing extensions in a natural laminar boundary layer wing region extending chordwise from said leading edge by a fraction of the chordlength of said wing and extending span-wise from opposing sides of said wing. Laminar flow control in other regions of the wing employs fuel stored in the wing as a coolant.
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