Publications & Works

Publication Network
Journal articles indexed in SCI, SSCI, and AHCI

Ablation Analyses of Optimized Nose Tips for Hypersonic Vehicles

Onay O. K., EYİ S.
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER , vol.34, no.1, pp.78-89, 2020 (SCI-Expanded) identifier identifier

Shape Optimization of Reentry Vehicles to Minimize Heat Loading

Eyi S., Hanquist K. M., Boyd I. D.
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER , vol.33, no.3, pp.785-796, 2019 (SCI-Expanded) identifier identifier

Aerothermodynamic Design Optimization of Hypersonic Vehicles

Eyi S., Hanquist K. M., Boyd I. D.
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER , vol.33, no.2, pp.392-406, 2019 (SCI-Expanded) identifier identifier

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

Rouzbar R., EYİ S.
AERONAUTICAL JOURNAL , vol.122, no.1258, pp.1884-1915, 2018 (SCI-Expanded) Sustainable Development identifier identifier

Aerothermodynamic shape optimization of hypersonic blunt bodies

EYİ S., Yumusak M.
ENGINEERING OPTIMIZATION , vol.47, no.7, pp.909-926, 2015 (SCI-Expanded) identifier identifier

Convergence Error and Higher-Order Sensitivity Estimations

Eyi S.
AIAA JOURNAL , vol.50, no.10, pp.2219-2234, 2012 (SCI-Expanded) identifier identifier

Design optimization of rocket nozzles in chemically reacting flows

Yumusak M., EYİ S.
COMPUTERS & FLUIDS , vol.65, pp.25-34, 2012 (SCI-Expanded) identifier identifier

Effects of sensitivity derivatives on aerodynamic design optimization

Eyi S.
Inverse Problems In Science And Engineering , vol.2, no.1996, pp.213-235, 2007 (SCI-Expanded)

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

Onur O., Eyi S.
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS , vol.49, no.2, pp.211-231, 2005 (SCI-Expanded) identifier identifier

Inverse airfoil design using the Navier Stokes equations

Eyi S., Lee K.
ENGINEERING OPTIMIZATION , vol.28, no.4, pp.245-262, 1997 (SCI-Expanded) identifier identifier

High-lift design optimization using Navier-Stokes equations

Eyi S., Lee K., Rogers S., Kwak D.
JOURNAL OF AIRCRAFT , vol.33, no.3, pp.499-504, 1996 (SCI-Expanded) identifier identifier

AIRFOIL DESIGN OPTIMIZATION USING THE NAVIER-STOKES EQUATIONS

EYI S., HAGER J., LEE K.
JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS , vol.83, no.3, pp.447-461, 1994 (SCI-Expanded) identifier identifier

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

HAGER J., EYI S., LEE K.
JOURNAL OF AIRCRAFT , vol.31, no.5, pp.1143-1147, 1994 (SCI-Expanded) identifier identifier

TRANSONIC AIRFOIL DESIGN BY CONSTRAINED OPTIMIZATION

LEE K., EYI S.
JOURNAL OF AIRCRAFT , vol.30, no.6, pp.805-806, 1993 (SCI-Expanded) identifier identifier

AERODYNAMIC DESIGN VIA OPTIMIZATION

LEE K., EYI S.
JOURNAL OF AIRCRAFT , vol.29, no.6, pp.1012-1019, 1992 (SCI-Expanded) identifier identifier
Articles Published in Other Journals

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

Özgün M., EYİ S.
Havacılık ve Uzay Teknolojileri Dergisi , vol.7, pp.71-77, 2014 (Peer-Reviewed Journal)
Papers Presented at Peer-Reviewed Scientific Conferences

ROKET KALKIŞ RAMPALARINDA EĞİM AÇISININ VE GEOMETRİNİN ETKİSİNİN İNCELENMESİ

Yahya L., Soylu Z. S., Eyi S.
10. ULUSAL HAVACILIK ve UZAY KONFERANSI, Ankara, Turkey, 18 - 20 September 2024, pp.1-11

FIRLATMA RAMPALARINDA ATEŞLEME AŞIRI BASINÇ DALGALARININ HAD ANALİZİ

Duru M. Ö., Eyi S.
10. ULUSAL HAVACILIK ve UZAY KONFERANSI, Ankara, Turkey, 18 - 20 September 2024, pp.1-10

BEŞİNCİ NESİL BİR SAVAŞ UÇAĞININ KAVRAMSAL TASARIMI: UÇUŞ MEKANİĞİ YAKLAŞIMI

Kırkar A., Eyi S.
10. ULUSAL HAVACILIK ve UZAY KONFERANSI, Ankara, Turkey, 18 - 20 September 2024, pp.1-11

Ignition Overpressure Analyses of Launch Pads at Different Deflector Angles

İriolya T. G., Eyi S.
12. International Conference on Computational Fluid Dynamics (ICCFD12), Kobe, Japan, 14 - 19 July 2024, no.6, pp.1-22 Creative Commons License

HIGH-FIDELITY NUMERICAL INVESTIGATION OF A HIGH PRESSURE TURBINE COOLED VANE

Gokenis F., Peneklioglu K., Oksuz O., Erdem E., EYİ S.
69th ASME Turbo Expo 2024: Turbomachinery Technical Conference and Exposition, GT 2024, London, England, 24 - 28 June 2024, vol.13 identifier

Numerical Modeling of Hypersonic Air and Carbon Dioxide Flows in Thermochemical Non-Equilibrium with SU2-NEMO Solver

Çelik M., Uğur Ö., Eyi S.
The 2nd International Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions Engineering (FAR), Heilbronn, Germany, 19 - 23 June 2022, pp.1-6 Creative Commons License

Computational modelling and analysis of porous bleed holes at supersonic speeds

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

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

Unlu T., Atasoy M., Dincer E., EYİ S.
10th Ankara International AerospaceConference, Ankara, Turkey, 18 - 20 September 2019, vol.10

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

Onay O., EYİ S.
10th Ankara International Aerospace Conference, Ankara, Turkey, 18 - 20 September 2019, vol.10, (Full Text)

Shape Optimization of Reentry Vehicles to Minimize Heat Loading

EYİ S., Hanquist K. M., Boyd I. D.
2019 AIAA Scitech Forum, San Diego, CA USA, 7 - 11 January 2019, vol.2019, (Full Text) identifier

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

Akar G., EYİ S.
VII. Ulusal Havacılık Ve Uzay Konferansı, Turkey, 12 - 14 September 2018, vol.2018

Aerothermodynamic Shape Optimization of Reentry Capsules Using DSMC and POD Methods

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

Aerothermodynamic Shape Optimization of Reentry Capsule

Kutkan H., EYİ S.
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

Gür B., EYİ S.
2018 Fluid Dynamics Conference, Atlanta, Georgia, 25 - 29 June 2018, vol.2018 identifier

Transient Thermochemical Erosion Modeling for Solid Propellant Rocket Motor Nozzles Including the Effect of Shape Change and Anisotropy

Onay O., EYİ S.
2018 Fluid Dynamics Conference, Atlanta, Georgia, 25 - 29 June 2018, vol.2018, (Full Text) identifier

Aerothermodynamic Design Optimization of Hypersonic Vehicles

EYİ S., Hanquist K. M., Boyd I. D.
2018 Multidisciplinary Analysis and Optimization Conference, Atlanta, Georgia, 25 - 29 June 2018, vol.2018 identifier

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

Özmen E., EYİ S.
2018 Fluid Dynamics Conference, Atlanta, Georgia, 25 - 29 June 2018, vol.2018 identifier

CFD Analysis of Diffusion Phenomena in Hypersonic Flow Regimes

Gür B., EYİ S.
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

Gur H. B., EYİ S.
AIAA Aerospace Sciences Meeting, 2018, Florida, United States Of America, 8 - 12 January 2018 identifier

Diffusion Models Implementation in Hypersonic Flow Regimes

Gür B., EYİ S.
9th Ankara International Aerospace Conference, 20 - 22 September 2017, vol.2017

Analysis of effects of different diffusion models in hypersonic flow regimes

Gur H. B., EYİ S.
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

YILDIRIM A., EYİ S.
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

Yıldırım A., EYİ S.
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

Rouzbar R., EYİ S.
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

Onay O., EYİ S.
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

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

Three Dimensional Design Optimization Using Adjoint Method

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

Convergence Acceleration Based on Eigenvalue Analysis

EYİ S.
46th AIAA Fluid Dynamics Conference, Washington, Kiribati, 13 - 17 June 2016, vol.2016, (Full Text) identifier

Modelling Thermochemical Nonequilibrium during Atmospheric Re-Entry

Pişkin T., EYİ S.
51st AIAA/SAE/ASEE Joint Propulsion Conference, Orlando, FL, 27 August - 27 September 2015, vol.2015, (Full Text) identifier

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

Özgün M., EYİ S.
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

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

Implicit Solution of One-Dimensional Transient Ablation

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

Simulations of Ethylene and Hydrogen Combustions in Scramjet Combustor

Rouzbar R., EYİ S.
51st AIAA/SAE/ASEE Joint Propulsion Conference, Orlando, FL, 27 July 2105 - 29 July 2015, vol.2015, (Full Text) identifier

Convergence Acceleration Using Convergence Error Estimation

EYİ S.
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

Rouzbar R., EYİ S.
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, 22 June 2105 - 26 June 2015, vol.2015, (Full Text) identifier

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

Muslubaş E., EYİ S.
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, 22 - 26 June 2015, vol.2015, (Full Text) identifier

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

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

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

Özgün M., EYİ S.
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

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

Analysis of hypersonic flow using three dimensional Navier-Stokes equations

Özgün M., EYİ S.
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

Piskin T., EYİ S., Yumusak M.
32nd AIAA Applied Aerodynamics Conference 2014, Atlanta, GA, United States Of America, 16 - 20 June 2014 identifier

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

Yildizlar B., EYİ S.
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

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

Analysis and adjoint design optimization of hypersonic blunt bodies

Piskin T., EYİ S.
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014, Ohio, United States Of America, 28 - 30 July 2014, (Full Text) identifier

Analysis and design optimization of three dimensional nozzles

Yildizlar B., EYİ S.
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

EYİ S.
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, San Jose, CA, United States Of America, 14 - 17 July 2013, (Full Text) identifier

Three dimensional rocket nozzle design using adjoint method

EYİ S., Yumusak M.
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

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

Aerothermodynamic Shape Optimization ofHypersonic Blunt Bodies

Yumusak M., EYİ S.
21st AIAA ComputationalFluid Dynamics Conference, 24 - 27 June 2013, vol.2013

Convergence acceleration based on convergence error estimation

EYİ S., Yumusak M.
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

EYİ S., Yumusak M.
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

EYİ S.
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

EYİ S., Yumuşak M.
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, 24 - 28 September 2012, (Full Text) identifier

Convergence Error Estimation and Convergence Acceleration in Iteratively Solved Problems

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

Three dimensional design optimization using analytical and numerical jacobians

EYİ S., Ezertas A., Degirmenci M., Yumusak M.
20th AIAA Computational Fluid Dynamics Conference 2011, Honolulu, HI, United States Of America, 27 - 30 June 2011 identifier

Design optimization in chemically reacting flows

Yumuşak M., EYİ S.
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

EYİ S.
20th AIAA Computational Fluid Dynamics Conference 2011, Honolulu, HI, United States Of America, 27 - 30 June 2011, (Full Text) identifier

Design Optimization in Non-equilibrium Reacting Flows

EYİ S., Ezertas A., Yumusak M.
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

Ezertas A., EYİ S.
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

Ezertaş A. A., EYİ S.
19th AIAA Computational Fluid Dynamics, San-Antonio, Northern Mariana Islands, 22 - 25 June 2009, vol.2009, (Full Text) identifier

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

Onur O., EYİ S.
17th AIAA Computational Fluid Dynamics Conference, Toronto, Canada, 6 - 09 June 2005 identifier

Inverse design of compressor cascades on parallel computers

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

Inverse design of compressor cascades

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

Effects of sensitivity analysis on turbomachinery blade design

Kocabiçak E., EYİ S.
35th Intersociety Energy Conversion Engineering Conference and Exhibit 2000, Las Vegas, NV, United States Of America, 24 - 28 July 2000, (Full Text) identifier

Aerodynamic sensitivity analysis in inverse design

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

Turbomachinery blade design via optimization

EYİ S., Lee K.
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

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

Transonic turbomachinery blade design using optimization

EYİ S., Lee K.
35th Aerospace Sciences Meeting and Exhibit, 1997, Nevada, United States Of America, 6 - 09 January 1997 identifier

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

Eyi S., Chand K., Lee K., Rogers S., Kwak D.
Fluid Dynamics Conference, 1996, Louisiana, United States Of America, 17 - 20 June 1996, pp.1-11 identifier

Efficiency improvement in sensitivity evaluation in aerodynamic shape optimization

Eyi S., Lee K.
14th Applied Aerodynamics Conference, 1996, Louisiana, United States Of America, 17 - 20 June 1996, pp.1022-1031, (Full Text) identifier

Effects of sensitivity analysis on aerodynamic design optimization

Eyi S., Lee K.
Proceedings of the 1995 ASME International Mechanical Congress and Exposition, San-Francisco, Costa Rica, 12 - 17 November 1995, vol.232, pp.1-8, (Full Text) identifier

High-lift design optimization using the Navier-Stokes equations

EYİ S., Lee K. D., Rogers S. E.
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

Hager J., Eyi S., Lee K.
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

Eyi S., Lee K.
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

Hager J., Eyi S., Lee K.
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

Lee K., Eyi S.
9th Applied Aerodynamics Conference, 1991, Maryland, United States Of America, 23 - 25 September 1991 identifier
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Publication

93

Citation (WoS)

133

H-Index (WoS)

7

Citation (Scopus)

225

H-Index (Scopus)

9

Citation (Scholar)

1

H-Index (Scholar)

1

Project

5

Thesis Advisory

36

Open Access

20
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