Hulya Sukas

Hulya Sukas
Istanbul Technical University · Department of Aeronautical Engineering

Master of Science

About

5
Publications
805
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3
Citations
Introduction
Hulya Sukas is currently a PhD student at the Department of Aeronautical Engineering, Istanbul Technical University. She graduated from Mechanical Engineering and Ocean Engineering in Yildiz Technical University.
Skills and Expertise
Computational Fluid Dynamics
Fluid Mechanics
Numerical Modeling
Aerodynamics
CFD Coding
Computational Fluid Mechanics
Numerical Simulation
Hydrodynamics
Programming in MATLAB
Numerical Analysis
Education
January 2017 - June 2019
Istanbul Technical University
Istanbul Technical University
Field of study
  • Aeronautical Engineering
September 2014 - January 2017
Yildiz Technical University
Yildiz Technical University
Field of study
  • Mechanical Engineering
September 2013 - December 2016
Yildiz Technical University
Yildiz Technical University
Field of study
  • Naval Architecture and Marine Engineering

Publications

Publications (5)
HEMLAB Algorithm Applied to 4th AIAA CFD High Lift Prediction Workshop
Conference Paper
  • Jun 2022
Figure 1: Flow chart for mesh adaptation process
Figure 2: Nearfield pressure signature on the z = −32.92 and y = 0
Figure 4: Streamtraces on the main body for inital mesh with SU2 [a]...
Figure 5: Nearfield pressure signature on the z = −32.92 and y = 0
+4 Figure 7: Wake region and sonic boom visualization at x=50
Prediction of the Nearfield Pressure Signature Using HEMLAB Algorithm
Conference Paper
Full-text available
  • Sep 2021
In this study, the NASA Concept 25D with Flow-Through Nacelle (C25F) proposed in the AIAA Sonic Boom Workshop has been studied in two different aspects. First part of this paper is about validating the vertex based finite volume algorithm named HEMLAB for the selected geometry in terms of aerodynamic forces and pressure signatures. The HEMLAB algor...
Figure 1. Three dimensional facet-edges [a], sym and rot pointers [b],...
Figure 6. High lift JAXA Standard Model (JSM) (Nacelle/Pylon-Off model,...
Figure 7. High lift JAXA Standard Model (JSM) approximate wing sections.
Figure 15. Computed entropy isosurface (∆s = 0.001) with a slice at x =...
+5 Figure 16. Computed y+ values for HEMLAB at M∞ = 0.172, Re = 1.93 × 10...
HEMLAB Algorithm Applied to the High-Lift JAXA Standard Model
Conference Paper
Full-text available
  • Jan 2021
The high-lift JAXA Standard Model (HL-JSM) has been numerically analyzed in order to further validate the HEMLAB code for realistic aircraft configurations. The numerical algorithm is based on highly efficient edge-based data structure for a vertex based finite volume algorithm on hybrid meshes. The data pattern is arranged to meet the requirements...
Figure 1: Planar and non-planar wing systems. Since there is a...
Figure 2: Main dimensions of half body of aircraft. Since the Eulerian...
Figure 6: Workflow diagram of the CFD based optimization study.
Figure 7: Lift (left) and drag (right) coefficients for different AoAs....
+5 Figure 10: Optimization variables for C-wing geometry.
AERODYNAMIC DESIGN OPTIMIZATION OF A NON-PLANAR C-WING CONFIGURATION
Conference Paper
Full-text available
  • Sep 2019
The main objective for aerodynamic design of an aerospace structure is to enhance aerodynamic performance of lifting surfaces, while a numerical optimization procedure driving this design process can contribute significantly to the desired outcomes. This paper presents a study on aerodynamic analysis and optimization applied to a non-planar wing st...
Table 2 . Boundary conditions imposed on the solver.
Table 4 .
Table 6 .
Main dimensions of the model size and full-scale ship.
An Adjoint Numerical / Empirical Approach to Predict the Total Resistance of Ships
Article
Full-text available
  • Dec 2018
This study aims to propose a fast calculation method to evaluate the total resistance of a traditional ship hull form. It became a common knowledge nowadays that the computational fluid dynamics (CFD) approach is robust in calculating the frictional resistance component of a ship with double body flow solutions. Modeling of the free surface is stil...