Aerofoil profile and sweep optimisation for a blended wing-body aircraft using a discrete adjoint method

Publisher: Cambridge University Press

E-ISSN: 2059-6464|110|1111|589-604

ISSN: 0001-9240

Source: The Aeronautical Journal, Vol.110, Iss.1111, 2006-09, pp. : 589-604

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Abstract