Comparison on the aerodynamic coefficients obtained from three different size of wind tunnel model on Baseline V set at 45 degree sweep tail angle
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...
Main Authors: | , , , , , , |
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Format: | Article |
Language: | English |
Published: |
Science Publishing Corporation Inc.
2018
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Subjects: | |
Online Access: | http://eprints.utm.my/86631/1/IskandarShah2018_ComparisonontheAerodynamicCoefficientsObtainedfromThree.pdf |