Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/5657
Title: Design and optimization of a supersonic business jet
Authors: Kıyıcı, F.
Aradağ, S.
Issue Date: 2015
Publisher: American Institute of Aeronautics and Astronautics Inc, AIAA
Source: 22nd AIAA Computational Fluid Dynamics Conference, 2015, 22 June 2015 through 26 June 2015, , 157389
Abstract: Supersonic transport (SST) technology has widely been investigated. Flow characteristics become complicated in supersonic conditions, and aerodynamic shape optimization studies are required for the design process of supersonic vehicles. An optimized aircraft is very efficient in terms of fuel consumption and pressure losses. This study focuses on the aerodynamic design and shape optimization of a supersonic business jet. For this purpose, a design algorithm (BF-I) is developed with the help of historical trends of supersonic aircrafts, commercial aircrafts and experimental correlations. After obtaining the baseline geometry, a gradient-based optimization is employed to get optimum results for the design. The developed numerical methodology is tested for both 2D and 3D geometries. CFD analysis are performed by using SU2 (Stanford University Unstructured) solver that has high performance for compressible flows. Euler equations are used for the analyses. © 2015, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
URI: https://doi.org/10.2514/6.2015-3064
https://hdl.handle.net/20.500.11851/5657
ISBN: 9781624103667
Appears in Collections:Makine Mühendisliği Bölümü / Department of Mechanical Engineering
Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection

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