Experimental investigation of center elevator deflection on aerodynamics of UiTM's Baseline-I Blended Wing Body (BWB) unmanned aerial vehicle (UAV)

Wirachman Wisnoe; M.A Zurriati; M Firdaus; R Nor Fazira; Rizal E.M. Nasir; Wahyu Kuntjoro

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https://doi.org/10.1109/cssr.2...

Article . 2010 . Peer-reviewed

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https://dx.doi.org/10.1109/css...

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Experimental investigation of center elevator deflection on aerodynamics of UiTM's Baseline-I Blended Wing Body (BWB) unmanned aerial vehicle (UAV)

descriptionPublicationkeyboard_double_arrow_right Article 01 Dec 2010Publisher:IEEEJournal:2010 International Conference on Science and Social Research (CSSR 2010)

Authors: Wirachman Wisnoe; M.A Zurriati; M Firdaus; R Nor Fazira; Rizal E.M. Nasir; Wahyu Kuntjoro;

doi: 10.1109/cssr.2010.5773694

Experimental investigation of center elevator deflection on aerodynamics of UiTM's Baseline-I Blended Wing Body (BWB) unmanned aerial vehicle (UAV)

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Abstract

This paper describes the wind tunnel testing of a Blended Wing Body (BWB)-Baseline I with elevator developed in Universiti Teknologi MARA (UiTM). The experiment work was carried out in UiTM low speed wind tunnel using 1∶7 scaled model of BWB at Mach 0.1. The testing is conducted for center elevator angle between −10° to +10° until stall angle. The result show similar trends with zero elevator deflection case in terms of lift curve, drag curve and pitching moment curves.

Related Organizations

Universiti Teknologi MARA
Malaysia
Universiti Teknologi MARA System
Malaysia

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