39th Aerospace Sciences Meeting and Exhibit 2001
DOI: 10.2514/6.2001-421
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Physical properties of Maskell's induced drag integral

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Cited by 13 publications
(6 citation statements)
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“…8 shows that the induced drag can be significantly reduced for low altitude when cant angle reaches values between δ = [−60 • , −30 • ]. It can be shown that external lift distribution with smooth variation better performs regarding induced drag [22]. Observing Fig.…”
Section: B Sensitivity To Flight Conditionsmentioning
confidence: 78%
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“…8 shows that the induced drag can be significantly reduced for low altitude when cant angle reaches values between δ = [−60 • , −30 • ]. It can be shown that external lift distribution with smooth variation better performs regarding induced drag [22]. Observing Fig.…”
Section: B Sensitivity To Flight Conditionsmentioning
confidence: 78%
“…One can observed that the lift is shifted more inward for the innermost hinge and that the lift variation close to the tip are stronger. As emphasized in [22] the induced drag evolves as the lift times its first derivative with respect to span which explains the strongest increase of drag for the large winglet.…”
Section: A Impact Of Hinge Line Locationmentioning
confidence: 90%
“…Maskell's formula only by a compressibility correction F ∇ρ which involves density gradients and variations. As S e extends further away from the body surface, this correction gradually vanishes while F KJ and F MSK respectively reduce to the incompressible Kutta-Joukowski theorem (see [5]) and the incompressible Maskell's formula (see [16][17][18][19]59]).…”
Section: Development Of An Invariant Formulation Embedding Classical ...mentioning
confidence: 99%
“…In the end it was shown that, in transonic flows, F ρl + F trans m ρ differs from the classical Kutta-Joukowski theorem and Maskell's formula only by a compressibility correction F ∇ρ which involves density gradients and variations. As S e extends further away from the body surface, this correction gradually vanishes while F KJ and F MSK respectively reduce to the incompressible Kutta-Joukowski theorem (see [5]) and the incompressible Maskell's formula (see [16][17][18][19]59]). As it happens, it was shown by several authors that the incompressible Kutta-Joukowski theorem can predict the lift in compressible flows [8,9,43].…”
Section: A Links With the Kutta-joukowski Lift Theorem And Maskell's ...mentioning
confidence: 99%