Comparison on the aerodynamic coefficients obtained from three different size of wind tunnel model on Baseline V set at 45 degree sweep tail angle

• Main Authors: Abd. Latif, Mohamad Zulfazli Arief, Mohd. Nasir, Rizal Effendy, Ahmad, Muhammad Aiman, Wisnoe, Wirachman, Kuntjoro, Wahyu, Ishak, Iskandar Shah, Saad, M. R. S.
• Format: Article
• Language: English
• Published: Science Publishing Corporation Inc. 2018
• Subjects: TJ Mechanical engineering and machinery
• Online Access: http://eprints.utm.my/id/eprint/86631/1/IskandarShah2018_ComparisonontheAerodynamicCoefficientsObtainedfromThree.pdf; http://eprints.utm.my/id/eprint/86631/; https://www.sciencepubco.com/index.php/ijet/article/view/22248

This paper analyzes the aerodynamic coefficients of a blended wing body, Baseline V which is equipped with 45° sweep tail angle. Base-line V is one of the Universiti Teknologi MARA (UiTM) Shah Alam Flight Test Technology Centre's blended wing body designs that have unique configuration as it us...