Paper Title:
The Effect of Canard on Aerodynamics of Blended Wing Body
  Abstract

This paper describes the wind tunnel testing of a Blended Wing Body (BWB) with rectangular canards and twisted wing (Baseline II E2 configuration) developed in Universiti Teknologi MARA (UiTM). The experiment work was carried out in UiTM low speed wind tunnel using 1:6 scaled model of BWB at Mach 0.1. The testing is conducted for canard’s deflection angle between 0° to +20. The results show by adding the canard surface to the BWB’s body, at 12 degree and higher angles of attack,α there will be a slight increment in lift. Maximum lift-to-drag ratio decreases with increasing canard surface deflection. Also, by adding the canard surface, the value of moment at zero lift,CM,0 is increased.

  Info
Periodical
Chapter
Chapter 22: Metrology and Measurement
Edited by
Wu Fan
Pages
4156-4160
DOI
10.4028/www.scientific.net/AMM.110-116.4156
Citation
M. A. Zurriati, K. Wahyu, W. Wisnoe, E.M. N. Rizal, "The Effect of Canard on Aerodynamics of Blended Wing Body", Applied Mechanics and Materials, Vols. 110-116, pp. 4156-4160, 2012
Online since
October 2011
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Price
$32.00
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