Publications & Works

Articles Published in Journals That Entered SCI, SSCI and AHCI Indexes

Ablation Analyses of Optimized Nose Tips for Hypersonic Vehicles

JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, vol.34, no.1, pp.78-89, 2020 (Journal Indexed in SCI) identifier identifier

Shape Optimization of Reentry Vehicles to Minimize Heat Loading

JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, vol.33, no.3, pp.785-796, 2019 (Journal Indexed in SCI) identifier identifier

Aerothermodynamic Design Optimization of Hypersonic Vehicles

JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, vol.33, no.2, pp.392-406, 2019 (Journal Indexed in SCI) identifier identifier

Reacting flow analysis of a cavity-based scramjet combustor using a Jacobian-free Newton-Krylov method

AERONAUTICAL JOURNAL, vol.122, no.1258, pp.1884-1915, 2018 (Journal Indexed in SCI) Sustainable Development identifier identifier

Aerothermodynamic shape optimization of hypersonic blunt bodies

ENGINEERING OPTIMIZATION, vol.47, no.7, pp.909-926, 2015 (Journal Indexed in SCI) identifier identifier

Convergence Error and Higher-Order Sensitivity Estimations

AIAA JOURNAL, vol.50, no.10, pp.2219-2234, 2012 (Journal Indexed in SCI) identifier identifier

Design optimization of rocket nozzles in chemically reacting flows

COMPUTERS & FLUIDS, vol.65, pp.25-34, 2012 (Journal Indexed in SCI) identifier identifier

Effects of sensitivity derivatives on aerodynamic design optimization

Inverse Problems In Science And Engineering, vol.2, no.1996, pp.213-235, 2007 (Journal Indexed in SCI)

Effects of the Jacobian evaluation on Newton's solution of the Euler equations

INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, vol.49, no.2, pp.211-231, 2005 (Journal Indexed in SCI) identifier identifier

Inverse airfoil design using the Navier Stokes equations

ENGINEERING OPTIMIZATION, vol.28, no.4, pp.245-262, 1997 (Journal Indexed in SCI) identifier identifier

High-lift design optimization using Navier-Stokes equations

JOURNAL OF AIRCRAFT, vol.33, no.3, pp.499-504, 1996 (Journal Indexed in SCI) identifier identifier

AIRFOIL DESIGN OPTIMIZATION USING THE NAVIER-STOKES EQUATIONS

JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS, vol.83, no.3, pp.447-461, 1994 (Journal Indexed in SCI) identifier identifier

2-POINT TRANSONIC AIRFOIL DESIGN USING OPTIMIZATION FOR IMPROVED OFF-DESIGN PERFORMANCE

JOURNAL OF AIRCRAFT, vol.31, no.5, pp.1143-1147, 1994 (Journal Indexed in SCI) identifier identifier

TRANSONIC AIRFOIL DESIGN BY CONSTRAINED OPTIMIZATION

JOURNAL OF AIRCRAFT, vol.30, no.6, pp.805-806, 1993 (Journal Indexed in SCI) identifier identifier

AERODYNAMIC DESIGN VIA OPTIMIZATION

JOURNAL OF AIRCRAFT, vol.29, no.6, pp.1012-1019, 1992 (Journal Indexed in SCI) identifier identifier

Articles Published in Other Journals

ATMOSFERİK GEÇİŞ YAPAN ARAÇ ETRAFINDA NAVIER-STOKESDENKLEMLERİ İLE ÜÇ BOYUTLU HİPERSONİK AKIŞ ANALİZİ

Havacılık ve Uzay Teknolojileri Dergisi, vol.7, pp.71-77, 2014 (Other Refereed National Journals)

Refereed Congress / Symposium Publications in Proceedings

Computational modelling and analysis of porous bleed holes at supersonic speeds

AIAA Propulsion and Energy 2020 Forum, Virtual, Online, 24 - 28 August 2020, pp.1-10 identifier

Comparison of Fully Coupled and DecoupledModeling Results of Graphite Ablation In Hypersonic Flows

10th Ankara International Aerospace Conference, Ankara, Turkey, 18 - 20 September 2019, vol.10

Integrated Shap Optimization of RAE-M2129 Inlet for Aerodynamic Performance and Reduced Radar Cross Section

10th Ankara International AerospaceConference, Ankara, Turkey, 18 - 20 September 2019, vol.10

Shape Optimization of Reentry Vehicles to Minimize Heat Loading

2019 AIAA Scitech Forum, San Diego, CA USA, 7 - 11 January 2019, vol.2019 identifier

Gözenekli Tahliye Sistemlerinin Ses-üstü Hızlarda Hesaplamalı Akışkanlar Dinamiği ile Analizleri

VII. Ulusal Havacılık Ve Uzay Konferansı, Turkey, 12 - 14 September 2018, vol.2018

Aerothermodynamic Shape Optimization of Reentry Capsules Using DSMC and POD Methods

10th NTERNATIONAL CONFERENCE ON COMPUTATIONAL FLUID DYNAMICS, 9 - 13 July 2018, vol.10

Aerothermodynamic Shape Optimization of Reentry Capsule

2018 Joint Thermophysics and Heat Transfer Conference, Atlanta, Georgia, 25 - 29 June 2018, vol.2018 identifier

CFD Analyses of Hypersonic Flow Regimes with Stephan-Maxwell Diffusion Equation

2018 Fluid Dynamics Conference, Atlanta, Georgia, 25 - 29 June 2018, vol.2018 identifier

Multi Block and Parallel Computations of Rotor Fan Using Three Dimensional Euler Equations

2018 Fluid Dynamics Conference, Atlanta, Georgia, 25 - 29 June 2018, vol.2018 identifier

Aerothermodynamic Design Optimization of Hypersonic Vehicles

2018 Multidisciplinary Analysis and Optimization Conference, Atlanta, Georgia, 25 - 29 June 2018, vol.2018 identifier

CFD Analysis of Diffusion Phenomena in Hypersonic Flow Regimes

26th Annual Conference of the Computational Fluid Dynamics Society of Canada Winnipeg, 10 - 12 June 2018, vol.26

Simulations of hypersonic flow regions with Fick’s law of diffusion with addition of different diffusivity models

AIAA Aerospace Sciences Meeting, 2018, Florida, United States Of America, 8 - 12 January 2018 identifier

Diffusion Models Implementation in Hypersonic Flow Regimes

9th Ankara International Aerospace Conference, 20 - 22 September 2017, vol.2017

Analysis of effects of different diffusion models in hypersonic flow regimes

8th AIAA Theoretical Fluid Mechanics Conference, 2017, Colorado, United States Of America, 5 - 09 June 2017 identifier

Aerodynamic optimization of wing-body configuration using discrete adjoint method

35th AIAA Applied Aerodynamics Conference, 2017, Colorado, United States Of America, 5 - 09 June 2017 identifier

Three Dimensional Design Optimization Using Adjoint Method with Newton Krylov Solver

52nd AIAA/SAE/ASEE Joint Propulsion Conference, Salt Lake City, UT, 25 - 27 July 2016, vol.2016 identifier

Scramjet Combustor Flow Analysis Using Coupled Navier-Stokes and Finite Rate Chemical Equations

46th AIAA Fluid Dynamics Conference, Washington, Kiribati, 13 - 17 July 2016, vol.2016 identifier

Adjoint Shape Optimization of Hypersonic Blunt BodiesIncluding the Effect of Graphite Ablation

Ninth International Conference onComputational Fluid Dynamics (ICCFD9), 11 - 15 July 2016, vol.9

Three Dimensional Hypersonic Flow Analysis Around a Reentry Vehicle Using Navier‐Stokes Equations

Ninth International Conference on Computational Fluid Dynamics (ICCFD9), 11 - 15 July 2016, vol.9

Three Dimensional Design Optimization Using Adjoint Method

34th AIAA Applied Aerodynamics Conference, Washington, Kiribati, 13 - 17 June 2016, vol.2016 identifier

Convergence Acceleration Based on Eigenvalue Analysis

46th AIAA Fluid Dynamics Conference, Washington, Kiribati, 13 - 17 June 2016, vol.2016 identifier

Modelling Thermochemical Nonequilibrium during Atmospheric Re-Entry

51st AIAA/SAE/ASEE Joint Propulsion Conference, Orlando, FL, 27 August - 27 September 2015, vol.2015 identifier

Hypersonic Flow Analysis of Re-entry Vehicles Using Three Dimensional Navier-Stokes Equations

13th International Energy Conversion Engineering Conference, Orlando, FL, 27 July 2105 - 29 July 2015, vol.2015 identifier

Implicit Solution of One-Dimensional Transient Ablation

13th International Energy Conversion Engineering Conference, Orlando, FL, 27 July 2105 - 29 July 2015, vol.2015 identifier

Diffusion Effect on Hypersonic Flow Using Fick’s Law

13th International Energy Conversion Engineering Conference, Orlando, FL, 27 - 20 July 2015, vol.2015 identifier

Simulations of Ethylene and Hydrogen Combustions in Scramjet Combustor

51st AIAA/SAE/ASEE Joint Propulsion Conference, Orlando, FL, 27 July 2105 - 29 July 2015, vol.2015 identifier

Convergence Acceleration Using Convergence Error Estimation

22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, 22 - 26 June 2015, vol.2015 identifier

Three Dimensional Flow Analysis of a Cavity-Based Scramjet Combustor

22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, 22 June 2105 - 26 June 2015, vol.2015 identifier

Analysis of Hypersonic Nozzles with Newton and Preconditioned Newton-GMRES Methods

51st AIAA/SAE/ASEE Joint Propulsion Conference, Orlando, FL, 22 June 2105 - 26 May 2016, vol.2015 identifier

Performances of Newton and Preconditioned Newton-GMRES Methods in Hypersonic Flow Solutions

22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, 22 - 26 June 2015, vol.2015 identifier

Three Dimensional Analysis of Hypersonic Flow Around Re-entry Vehicles Using Navier-Stokes Equations

7th International Conference on Recent Advances in Space Technologies, RAST 2015, 16 - 19 June 2015

The Effects of Static Aeroelasticity on the Performance of Supersonic/Hypersonic Nozzles

44th AIAA Fluid Dynamics Conference, AIAA AVIATION Forum, Atlanta, Georgia, United States Of America, 16 - 20 June 2014, vol.2014 identifier

Comparison of newton and newton-GMRES methods for three dimensional supersonic nozzle design

32nd AIAA Applied Aerodynamics Conference 2014, Atlanta, GA, United States Of America, 16 - 20 June 2014 identifier

Analysis and adjoint design optimization of hypersonic blunt bodies

50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014, Ohio, United States Of America, 28 - 30 July 2014 identifier

Analysis and design optimization of blunt bodies in hypersonic flow

32nd AIAA Applied Aerodynamics Conference 2014, Atlanta, GA, United States Of America, 16 - 20 June 2014 identifier

Static aeroelastic analysis of supersonic nozzles and performance response

50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014, Ohio, United States Of America, 28 - 30 July 2014 identifier

Analysis of hypersonic flow using three dimensional Navier-Stokes equations

50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014, Ohio, United States Of America, 28 - 30 July 2014 identifier

Analysis and design optimization of three dimensional nozzles

50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014, Ohio, United States Of America, 28 - 30 July 2014 identifier

Aerothermodynamic design optimization in hypersonic flows

49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, San Jose, CA, United States Of America, 14 - 17 July 2013 identifier

Three dimensional rocket nozzle design using adjoint method

49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, San Jose, CA, United States Of America, 14 - 17 July 2013 identifier

Aerodynamic design optimization of three dimensional rocket nozzles using adjoint method

21st AIAA Computational Fluid Dynamics Conference, San Diego, CA, United States Of America, 24 - 27 June 2013 identifier

Aerothermodynamic Shape Optimization ofHypersonic Blunt Bodies

21st AIAA ComputationalFluid Dynamics Conference, 24 - 27 June 2013, vol.2013

Convergence acceleration based on convergence error estimation

21st AIAA Computational Fluid Dynamics Conference, San Diego, CA, United States Of America, 24 - 27 June 2013 identifier

Three dimensional rocket nozzle design using adjoint method

49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, JPC 2013, California, United States Of America, 14 - 17 July 2013 identifier

Aerothermodynamic design optimization in hypersonic flows

49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, JPC 2013, California, United States Of America, 14 - 17 July 2013 identifier

Design optimization in hypersonic flows

18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, 24 - 28 September 2012 identifier

Convergence Error Estimation and Convergence Acceleration in Iteratively Solved Problems

7th International Conference on CFD (ICCFD7), Big Island, Hawaii, United States Of America, 9 - 13 July 2012, vol.7 identifier

Design optimization in chemically reacting flows

20th AIAA Computational Fluid Dynamics Conference 2011, Honolulu, HI, United States Of America, 27 - 30 June 2011 identifier

Three dimensional design optimization using analytical and numerical jacobians

20th AIAA Computational Fluid Dynamics Conference 2011, Honolulu, HI, United States Of America, 27 - 30 June 2011 identifier

Finite-Difference Sensitivity Calculation in Iteratively Solved Problems

20th AIAA Computational Fluid Dynamics Conference 2011, Honolulu, HI, United States Of America, 27 - 30 June 2011 identifier

Design Optimization in Non-equilibrium Reacting Flows

6th International Conference on Computational Fluid Dynamics (ICCFD), St Petersburg, Russia, 12 - 16 July 2010, pp.247-248 identifier

Performance Evaluation of the Numerical Flux Jacobians in Flow Solution and Aerodynamic Design Optimization

6th International Conference on Computational Fluid Dynamics (ICCFD), St Petersburg, Russia, 12 - 16 July 2010, pp.241-246 identifier

Performances of Numerical and Analytical Jacobians in Flow and Sensitivity Analysis

19th AIAA Computational Fluid Dynamics, San-Antonio, Northern Mariana Islands, 22 - 25 June 2009, vol.2009 identifier

Effects of the Jacobian evaluation on Newton's solution of the Euler equations

17th AIAA Computational Fluid Dynamics Conference, Toronto, Canada, 6 - 09 June 2005 identifier

Inverse design of compressor cascades on parallel computers

40th AIAA Aerospace Sciences Meeting and Exhibit 2002, Reno, NV, United States Of America, 14 - 17 January 2002 identifier

Inverse design of compressor cascades

39th Aerospace Sciences Meeting and Exhibit 2001, Reno, NV, United States Of America, 8 - 11 January 2001 identifier

Aerodynamic sensitivity analysis in inverse design

8th Symposium on Multidisciplinary Analysis and Optimization 2000, Long Beach, CA, United States Of America, 6 - 08 September 2000 identifier

Effects of sensitivity analysis on turbomachinery blade design

35th Intersociety Energy Conversion Engineering Conference and Exhibit 2000, Las Vegas, NV, United States Of America, 24 - 28 July 2000 identifier

Turbomachinery blade design via optimization

38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, United States Of America, 10 - 13 January 2000 identifier

Effects of sensitivity analysis on airfoil design

36th AIAA Aerospace Sciences Meeting and Exhibit, 1998, Nevada, United States Of America, 12 - 15 January 1998 identifier

Transonic turbomachinery blade design using optimization

35th Aerospace Sciences Meeting and Exhibit, 1997, Nevada, United States Of America, 6 - 09 January 1997 identifier

Efficiency improvement in sensitivity evaluation in aerodynamic shape optimization

14th Applied Aerodynamics Conference, 1996, Louisiana, United States Of America, 17 - 20 June 1996, pp.1022-1031 identifier

Multi-element high-lift design using the Navier-Stokes equations

Fluid Dynamics Conference, 1996, Louisiana, United States Of America, 17 - 20 June 1996, pp.1-11 identifier

Effects of sensitivity analysis on aerodynamic design optimization

Proceedings of the 1995 ASME International Mechanical Congress and Exposition, San-Francisco, Costa Rica, 12 - 17 November 1995, vol.232, pp.1-8 identifier

High-lift design optimization using the Navier-Stokes equations

33rd Aerospace Sciences Meeting and Exhibit, Reno,NV,U.S.A., 9 - 12 January 1995, vol.1995 identifier

Design efficiency evaluation for transonic airfoil optimization: A case for Navier-Stokes design

AIAA 23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference, 1993, Florida, United States Of America, 6 - 09 July 1993 identifier

Inverse airfoil design using the Navier-stokes equations

AIAA/AHS/ASEE Aerospace Design Conference, 1993, California, United States Of America, 16 - 19 February 1993 identifier

A multi-point optimization for transonic airfoil design

4th Symposium on Multidisciplinary Analysis and Optimization, 1992, Ohio, United States Of America, 21 - 23 September 1992, pp.13-20 identifier

Transonic airfoil design by constrained optimization

9th Applied Aerodynamics Conference, 1991, Maryland, United States Of America, 23 - 25 September 1991 identifier