Items where Author is "NASIR, RIZAL EFFENDY BIN MOHD"

NASIR, RIZAL EFFENDY BIN MOHD (2010) Finite Element Analysis of Frame Profiles for the Development of Static Wing Box Test Rig. In: UNSPECIFIED.

NASIR, RIZAL EFFENDY BIN MOHD (2010) Wind Tunnel Experiments of UiTM BWB Baseline-I And Baseline-II UAV At 0.1 Mach Number. In: UNSPECIFIED.

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.

NASIR, RIZAL EFFENDY BIN MOHD (2010) Experimental Results Analysis of UiTM BWB Baseline-I and Baseline-II UAV Running at 0.1 Mach Number. In: UNSPECIFIED UNSPECIFIED.

NASIR, RIZAL EFFENDY BIN MOHD (2009) Aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) Using Computational Fluid Dynamics (CFD).

NASIR, RIZAL EFFENDY BIN MOHD (2005) Experimental Results Analysis of UiTM BWB Baseline-I and Baseline-II UAV Running at 0.1 Mach Number. ISSN 1675-9885

NASIR, RIZAL EFFENDY BIN MOHD (2009) Design and Development of Lab-Based Wing Test Rig for Static Test. In: UNSPECIFIED.

NASIR, RIZAL EFFENDY BIN MOHD (2005) Implementation of Topology Optimisation for Thermoelastic Problems in ANSYS Environment and its Application to the Design of Turbine Disc Cross-Section. In: UNSPECIFIED.

NASIR, RIZAL EFFENDY BIN MOHD (2007) The Design and Aerodynamics of Blended Wing Body (BWB) of Unmanned Aerial Vehicle (UAV) Using Computational Fluid Dynamics (CFD). In: UNSPECIFIED.

NASIR, RIZAL EFFENDY BIN MOHD (2007) Aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) Using Computational Fluid Dynamics (CFD). In: UNSPECIFIED.

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.

NASIR, RIZAL EFFENDY BIN MOHD (2008) Aerodynamics of Sub-Sonic Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) Using Computational Fluid Dynamics (CFD). In: UNSPECIFIED.