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Preliminary Design of �Baseline-II� Blended Wing-Body (BWB) Unmanned Aerial Vehicle (UAV): Achieving Higher Aerodynamic Efficiency Through Planform Redesign and Low-Fidelity Inverse Twist Method

NASIR, RIZAL EFFENDY BIN MOHD (2010) Preliminary Design of �Baseline-II� Blended Wing-Body (BWB) Unmanned Aerial Vehicle (UAV): Achieving Higher Aerodynamic Efficiency Through Planform Redesign and Low-Fidelity Inverse Twist Method. In: UNSPECIFIED.

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Item Type: Conference or Workshop Item (UNSPECIFIED)
PRISMA ID: 26819
URI: http://oarr.uitm.edu.my/id/eprint/26505

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