publication . Article . Other literature type . 2011

Application of Fuzzy Logic Approach for an Aircraft Model with and without Winglet

Hossain, A.; Rahman, A.; Dr. Md. Jakir Hossen; Iqbal, A. K. M. P.; Hasan, S. K.;
Open Access English
  • Published: 27 Mar 2011
Abstract
The measurement of aerodynamic forces and moments acting on an aircraft model is important for the development of wind tunnel measurement technology to predict the performance of the full scale vehicle. The potentials of an aircraft model with and without winglet and aerodynamic characteristics with NACA wing No. 65-3- 218 have been studied using subsonic wind tunnel of 1 m × 1 m rectangular test section and 2.5 m long of Aerodynamics Laboratory Faculty of Engineering (University Putra Malaysia). Focusing on analyzing the aerodynamic characteristics of the aircraft model, two main issues are studied in this paper. First, a six component wind tunnel external bala...
Subjects
free text keywords: Wind tunnel; Winglet; Lift coefficient; Fuzzy logic.
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ZENODO
Article . 2011
Provider: ZENODO
Zenodo
Other literature type . 2011
Provider: Datacite
Zenodo
Other literature type . 2011
Provider: Datacite
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