The following information was submitted:
Transactions: INTERNATIONAL JOURNAL of MECHANICS
Transactions ID Number: 19-450
Full Name: Wirachman Wisnoe
Position: Associate Professor
Age: ON
Sex: Male
Address: Universiti Teknologi MARA (UiTM), Faculty of Mech. Engineering, 40450 Shah Alam, Selangor
Country: MALAYSIA
Tel: +60-13-2733231
Tel prefix:
Fax: +60-3-55435160
E-mail address: wira_wisnoe@yahoo.com
Other E-mails: wira_wisnoe@salam.uitm.edu.my
Title of the Paper: Experimental Results Analysis for UiTM BWB Baseline-I and Baseline-II UAV Running at 0.1 Mach number
Authors as they appear in the Paper: Wirachman Wisnoe, Wahyu Kuntjoro, Firdaus Mohamad, Rizal Effendy Mohd Nasir, Nor F Reduan, Zurriati Ali
Email addresses of all the authors: wira_wisnoe@yahoo.com, wkuntjoro@yahoo.com, pee_adw@yahoo.com, fendy117@gmail.com, norfazira@gmail.com, zurrie_adik@yahoo.com
Number of paper pages: 10
Abstract: This paper presents results analysis for two models of UiTM Blended Wing Body (BWB) UAV tested in UiTM Low Speed Wind Tunnel. The first model is known as the BWB Baseline-I and the new model known as BWB Baseline-II. The Baseline-II has a simpler planform, broader-chord wing and slimmer body compared to its predecessor while maintaining wingspan. The wind-tunnel experiments were executed at around 0.1 Mach number or about 35m/s with 1/6 scaled down model. Baseline-I is designed with centre elevator while Baseline-II uses canard for pitching motion purpose. The experiments were carried out at various elevator and canard deflection angles. The lift coefficient, drag coefficient, pitching moment coefficient, L/D ratio and drag polar curves were plotted to show the performance of aircraft at various angle of attack. For zero elevator and canard deflection the results show similar trends in terms of lift curve, drag curve and pitching moment curves for both aircrafts.
Keywords: Aerodynamics, Blended Wing Body, Unmanned Aerial Vehicle, Wind Tunnel
EXTENSION of the file: .doc
Special (Invited) Session: Experimental Results Analysis for UiTM BWB Baseline-I and Baseline-II UAV Running at 0.1 Mach number
Organizer of the Session: 647-154
How Did you learn about congress: Associate Prof. Dr. P.A. Aswatha Narayana (paa_iitm@yahoo.co.in)
IP ADDRESS: 118.100.179.144
