A feasiblity study on designing model support systems for a blended wing body configuration in a transonic wind tunnel

Publisher： Cambridge University Press

E-ISSN： 2059-6464|110|1103|53-62

ISSN： 0001-9240

Source： The Aeronautical Journal, Vol.110, Iss.1103, 2006-01, pp. : 53-62

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