Home About Browse Policies Statistics

The Effect of Centre Elevator Deflection on Aerodynamics of UiTM Baseline-1 Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) at Mach 0.3 using Computational Fluid Dynamics

NASIR, RIZAL EFFENDY BIN MOHD (2009) The Effect of Centre Elevator Deflection on Aerodynamics of UiTM Baseline-1 Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) at Mach 0.3 using Computational Fluid Dynamics. In: UNSPECIFIED.

Full text not available from this repository.

Metadata

Item Type: Conference or Workshop Item (UNSPECIFIED)
PRISMA ID: 15891
URI: http://oarr.uitm.edu.my/id/eprint/22829

Actions (login required)

View Item
View Item

Citation