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.
Full text not available from this repository.Metadata
Item Type: | Conference or Workshop Item (UNSPECIFIED) |
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PRISMA ID: | 26819 |
URI: | http://oarr.uitm.edu.my/id/eprint/26505 |