Yayınlar & Eserler

SCI, SSCI ve AHCI İndekslerine Giren Dergilerde Yayınlanan Makaleler

Ablation Analyses of Optimized Nose Tips for Hypersonic Vehicles

JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, cilt.34, sa.1, ss.78-89, 2020 (SCI İndekslerine Giren Dergi) identifier identifier

Shape Optimization of Reentry Vehicles to Minimize Heat Loading

JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, cilt.33, sa.3, ss.785-796, 2019 (SCI İndekslerine Giren Dergi) identifier identifier

Aerothermodynamic Design Optimization of Hypersonic Vehicles

JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, cilt.33, sa.2, ss.392-406, 2019 (SCI İndekslerine Giren Dergi) identifier identifier

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

AERONAUTICAL JOURNAL, cilt.122, sa.1258, ss.1884-1915, 2018 (SCI İndekslerine Giren Dergi) identifier identifier

Aerothermodynamic shape optimization of hypersonic blunt bodies

ENGINEERING OPTIMIZATION, cilt.47, sa.7, ss.909-926, 2015 (SCI İndekslerine Giren Dergi) identifier identifier

Convergence Error and Higher-Order Sensitivity Estimations

AIAA JOURNAL, cilt.50, sa.10, ss.2219-2234, 2012 (SCI İndekslerine Giren Dergi) identifier identifier

Design optimization of rocket nozzles in chemically reacting flows

COMPUTERS & FLUIDS, cilt.65, ss.25-34, 2012 (SCI İndekslerine Giren Dergi) identifier identifier

Effects of sensitivity derivatives on aerodynamic design optimization

Inverse Problems In Science And Engineering, cilt.2, sa.1996, ss.213-235, 2007 (SCI İndekslerine Giren Dergi)

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

INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, cilt.49, sa.2, ss.211-231, 2005 (SCI İndekslerine Giren Dergi) identifier identifier

Inverse airfoil design using the Navier Stokes equations

ENGINEERING OPTIMIZATION, cilt.28, sa.4, ss.245-262, 1997 (SCI İndekslerine Giren Dergi) identifier identifier

High-lift design optimization using Navier-Stokes equations

JOURNAL OF AIRCRAFT, cilt.33, sa.3, ss.499-504, 1996 (SCI İndekslerine Giren Dergi) identifier identifier

AIRFOIL DESIGN OPTIMIZATION USING THE NAVIER-STOKES EQUATIONS

JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS, cilt.83, sa.3, ss.447-461, 1994 (SCI İndekslerine Giren Dergi) identifier identifier

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

JOURNAL OF AIRCRAFT, cilt.31, sa.5, ss.1143-1147, 1994 (SCI İndekslerine Giren Dergi) identifier identifier

TRANSONIC AIRFOIL DESIGN BY CONSTRAINED OPTIMIZATION

JOURNAL OF AIRCRAFT, cilt.30, sa.6, ss.805-806, 1993 (SCI İndekslerine Giren Dergi) identifier identifier

AERODYNAMIC DESIGN VIA OPTIMIZATION

JOURNAL OF AIRCRAFT, cilt.29, sa.6, ss.1012-1019, 1992 (SCI İndekslerine Giren Dergi) identifier identifier

Diğer Dergilerde Yayınlanan Makaleler

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

Havacılık ve Uzay Teknolojileri Dergisi, cilt.7, ss.71-77, 2014 (Diğer Kurumların Hakemli Dergileri)

Hakemli Kongre / Sempozyum Bildiri Kitaplarında Yer Alan Yayınlar

Computational modelling and analysis of porous bleed holes at supersonic speeds

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

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

10th Ankara International Aerospace Conference, Ankara, Türkiye, 18 - 20 Eylül 2019, cilt.10

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

10th Ankara International AerospaceConference, Ankara, Türkiye, 18 - 20 Eylül 2019, cilt.10

Shape Optimization of Reentry Vehicles to Minimize Heat Loading

2019 AIAA Scitech Forum, San Diego, CA USA, 7 - 11 Ocak 2019, cilt.2019 identifier

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

VII. Ulusal Havacılık Ve Uzay Konferansı, Türkiye, 12 - 14 Eylül 2018, cilt.2018

Aerothermodynamic Shape Optimization of Reentry Capsules Using DSMC and POD Methods

10th NTERNATIONAL CONFERENCE ON COMPUTATIONAL FLUID DYNAMICS, 9 - 13 Temmuz 2018, cilt.10

Aerothermodynamic Shape Optimization of Reentry Capsule

2018 Joint Thermophysics and Heat Transfer Conference, Atlanta, Georgia, 25 - 29 Haziran 2018, cilt.2018 identifier

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

2018 Fluid Dynamics Conference, Atlanta, Georgia, 25 - 29 Haziran 2018, cilt.2018 identifier

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

2018 Fluid Dynamics Conference, Atlanta, Georgia, 25 - 29 Haziran 2018, cilt.2018 identifier

Aerothermodynamic Design Optimization of Hypersonic Vehicles

2018 Multidisciplinary Analysis and Optimization Conference, Atlanta, Georgia, 25 - 29 Haziran 2018, cilt.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 Haziran 2018, cilt.26

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

AIAA Aerospace Sciences Meeting, 2018, Florida, Amerika Birleşik Devletleri, 8 - 12 Ocak 2018 identifier

Diffusion Models Implementation in Hypersonic Flow Regimes

9th Ankara International Aerospace Conference, 20 - 22 Eylül 2017, cilt.2017

Analysis of effects of different diffusion models in hypersonic flow regimes

8th AIAA Theoretical Fluid Mechanics Conference, 2017, Colorado, Amerika Birleşik Devletleri, 5 - 09 Haziran 2017 identifier

Aerodynamic optimization of wing-body configuration using discrete adjoint method

35th AIAA Applied Aerodynamics Conference, 2017, Colorado, Amerika Birleşik Devletleri, 5 - 09 Haziran 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 Temmuz 2016, cilt.2016 identifier

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

46th AIAA Fluid Dynamics Conference, Washington, Kiribati, 13 - 17 Temmuz 2016, cilt.2016 identifier

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

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

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

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

Three Dimensional Design Optimization Using Adjoint Method

34th AIAA Applied Aerodynamics Conference, Washington, Kiribati, 13 - 17 Haziran 2016, cilt.2016 identifier

Convergence Acceleration Based on Eigenvalue Analysis

46th AIAA Fluid Dynamics Conference, Washington, Kiribati, 13 - 17 Haziran 2016, cilt.2016 identifier

Modelling Thermochemical Nonequilibrium during Atmospheric Re-Entry

51st AIAA/SAE/ASEE Joint Propulsion Conference, Orlando, FL, 27 Ağustos - 27 Eylül 2015, cilt.2015 identifier

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

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

Implicit Solution of One-Dimensional Transient Ablation

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

Diffusion Effect on Hypersonic Flow Using Fick’s Law

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

Simulations of Ethylene and Hydrogen Combustions in Scramjet Combustor

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

Convergence Acceleration Using Convergence Error Estimation

22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, 22 - 26 Haziran 2015, cilt.2015 identifier

Three Dimensional Flow Analysis of a Cavity-Based Scramjet Combustor

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

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

51st AIAA/SAE/ASEE Joint Propulsion Conference, Orlando, FL, 22 Haziran 2105 - 26 Mayıs 2016, cilt.2015 identifier

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

22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, 22 - 26 Haziran 2015, cilt.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 Haziran 2015

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

44th AIAA Fluid Dynamics Conference, AIAA AVIATION Forum, Atlanta, Georgia, Amerika Birleşik Devletleri, 16 - 20 Haziran 2014, cilt.2014 identifier

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

32nd AIAA Applied Aerodynamics Conference 2014, Atlanta, GA, Amerika Birleşik Devletleri, 16 - 20 Haziran 2014 identifier

Analysis and adjoint design optimization of hypersonic blunt bodies

50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014, Ohio, Amerika Birleşik Devletleri, 28 - 30 Temmuz 2014 identifier

Analysis and design optimization of blunt bodies in hypersonic flow

32nd AIAA Applied Aerodynamics Conference 2014, Atlanta, GA, Amerika Birleşik Devletleri, 16 - 20 Haziran 2014 identifier

Static aeroelastic analysis of supersonic nozzles and performance response

50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014, Ohio, Amerika Birleşik Devletleri, 28 - 30 Temmuz 2014 identifier

Analysis of hypersonic flow using three dimensional Navier-Stokes equations

50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014, Ohio, Amerika Birleşik Devletleri, 28 - 30 Temmuz 2014 identifier

Analysis and design optimization of three dimensional nozzles

50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014, Ohio, Amerika Birleşik Devletleri, 28 - 30 Temmuz 2014 identifier

Aerothermodynamic design optimization in hypersonic flows

49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, San Jose, CA, Amerika Birleşik Devletleri, 14 - 17 Temmuz 2013 identifier

Three dimensional rocket nozzle design using adjoint method

49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, San Jose, CA, Amerika Birleşik Devletleri, 14 - 17 Temmuz 2013 identifier

Aerodynamic design optimization of three dimensional rocket nozzles using adjoint method

21st AIAA Computational Fluid Dynamics Conference, San Diego, CA, Amerika Birleşik Devletleri, 24 - 27 Haziran 2013 identifier

Aerothermodynamic Shape Optimization ofHypersonic Blunt Bodies

21st AIAA ComputationalFluid Dynamics Conference, 24 - 27 Haziran 2013, cilt.2013

Convergence acceleration based on convergence error estimation

21st AIAA Computational Fluid Dynamics Conference, San Diego, CA, Amerika Birleşik Devletleri, 24 - 27 Haziran 2013 identifier

Three dimensional rocket nozzle design using adjoint method

49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, JPC 2013, California, Amerika Birleşik Devletleri, 14 - 17 Temmuz 2013 identifier

Aerothermodynamic design optimization in hypersonic flows

49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, JPC 2013, California, Amerika Birleşik Devletleri, 14 - 17 Temmuz 2013 identifier

Design optimization in hypersonic flows

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

Convergence Error Estimation and Convergence Acceleration in Iteratively Solved Problems

7th International Conference on CFD (ICCFD7), Big Island, Hawaii, Amerika Birleşik Devletleri, 9 - 13 Temmuz 2012, cilt.7 identifier

Design optimization in chemically reacting flows

20th AIAA Computational Fluid Dynamics Conference 2011, Honolulu, HI, Amerika Birleşik Devletleri, 27 - 30 Haziran 2011 identifier

Three dimensional design optimization using analytical and numerical jacobians

20th AIAA Computational Fluid Dynamics Conference 2011, Honolulu, HI, Amerika Birleşik Devletleri, 27 - 30 Haziran 2011 identifier

Finite-Difference Sensitivity Calculation in Iteratively Solved Problems

20th AIAA Computational Fluid Dynamics Conference 2011, Honolulu, HI, Amerika Birleşik Devletleri, 27 - 30 Haziran 2011 identifier

Design Optimization in Non-equilibrium Reacting Flows

6th International Conference on Computational Fluid Dynamics (ICCFD), St Petersburg, Rusya, 12 - 16 Temmuz 2010, ss.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, Rusya, 12 - 16 Temmuz 2010, ss.241-246 identifier

Performances of Numerical and Analytical Jacobians in Flow and Sensitivity Analysis

19th AIAA Computational Fluid Dynamics, San-Antonio, Kuzey Mariana Adaları, 22 - 25 Haziran 2009, cilt.2009 identifier

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

17th AIAA Computational Fluid Dynamics Conference, Toronto, Kanada, 6 - 09 Haziran 2005 identifier

Inverse design of compressor cascades on parallel computers

40th AIAA Aerospace Sciences Meeting and Exhibit 2002, Reno, NV, Amerika Birleşik Devletleri, 14 - 17 Ocak 2002 identifier

Inverse design of compressor cascades

39th Aerospace Sciences Meeting and Exhibit 2001, Reno, NV, Amerika Birleşik Devletleri, 8 - 11 Ocak 2001 identifier

Aerodynamic sensitivity analysis in inverse design

8th Symposium on Multidisciplinary Analysis and Optimization 2000, Long Beach, CA, Amerika Birleşik Devletleri, 6 - 08 Eylül 2000 identifier

Effects of sensitivity analysis on turbomachinery blade design

35th Intersociety Energy Conversion Engineering Conference and Exhibit 2000, Las Vegas, NV, Amerika Birleşik Devletleri, 24 - 28 Temmuz 2000 identifier

Turbomachinery blade design via optimization

38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, Amerika Birleşik Devletleri, 10 - 13 Ocak 2000 identifier

Effects of sensitivity analysis on airfoil design

36th AIAA Aerospace Sciences Meeting and Exhibit, 1998, Nevada, Amerika Birleşik Devletleri, 12 - 15 Ocak 1998 identifier

Transonic turbomachinery blade design using optimization

35th Aerospace Sciences Meeting and Exhibit, 1997, Nevada, Amerika Birleşik Devletleri, 6 - 09 Ocak 1997 identifier

Efficiency improvement in sensitivity evaluation in aerodynamic shape optimization

14th Applied Aerodynamics Conference, 1996, Louisiana, Amerika Birleşik Devletleri, 17 - 20 Haziran 1996, ss.1022-1031 identifier

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

Fluid Dynamics Conference, 1996, Louisiana, Amerika Birleşik Devletleri, 17 - 20 Haziran 1996, ss.1-11 identifier

Effects of sensitivity analysis on aerodynamic design optimization

Proceedings of the 1995 ASME International Mechanical Congress and Exposition, San-Francisco, Kostarika, 12 - 17 Kasım 1995, cilt.232, ss.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 Ocak 1995, cilt.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, Amerika Birleşik Devletleri, 6 - 09 Temmuz 1993 identifier

Inverse airfoil design using the Navier-stokes equations

AIAA/AHS/ASEE Aerospace Design Conference, 1993, California, Amerika Birleşik Devletleri, 16 - 19 Şubat 1993 identifier

A multi-point optimization for transonic airfoil design

4th Symposium on Multidisciplinary Analysis and Optimization, 1992, Ohio, Amerika Birleşik Devletleri, 21 - 23 Eylül 1992, ss.13-20 identifier

Transonic airfoil design by constrained optimization

9th Applied Aerodynamics Conference, 1991, Maryland, Amerika Birleşik Devletleri, 23 - 25 Eylül 1991 identifier