Wave drag of cylindrical leading edge of slipping swept wing, and its dependence on angle of attack and angle of sweepback are investigated; it is shown that leading edge wave drag of swept wings and delta wings increases considerably when sweepback exceeds 30° of arc.
Drag of blunt leading edge of swept wing in hypersonic flow
Soprotivlenie strelovidnoi zatuplennoi kromki kryla pri giperzvukovykh skorostyakh
1964
3 pages
Aufsatz (Zeitschrift)
Russisch
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THE BLUNT-LEADING-EDGE PROBLEM IN HYPERSONIC FLOW
AIAA | 1963
|Hypersonic minimum drag forebodies with blunt leading edges
Online Contents | 2013
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