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- W2001776421 abstract "If dependence of drag D on lift L is suppressed by calculating the induced drag corresponding to L weight W, the minimum-time climb path, obtained either by the energy state analysis or by Green's Theorem, leads, as is well known, to discontinuities in the flight-path angle 7. This requires, of course, an unreasonable increase in lift, positive or negative! If the reciprocal of maximum L/D is treated as a small parameter e, dependent on Mach number, a more complete analysis reveals that the discontinuities in 7 are replaced by transitional boundary layers on time scales of order e l / 2 , during which L/D is of order e ~ //: rather than e ~." @default.
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- W2001776421 date "1977-08-01" @default.
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- W2001776421 title "Optimal Flight-Path-Angle Transitions in Minimum-Time Airplane Climbs" @default.
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- W2001776421 doi "https://doi.org/10.2514/3.58853" @default.
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