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Kirill S. Anisimov,Andrey A. Savelyev,Innocentiy A. Kursakov,Alexander V. Lysenkov,Prajwal S. Prakasha
Pág. 93 - 97
Nacelle shape optimization for Blended Wing Body (BWB) is performed. The optimization procedure is based on numerical calculations of the Reynolds?averaged Navier?Stokes equations. For the Top Level Aircraft Requirements, formulated in AGILE project, the...
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