Prof. SİNAN EYİ

AERONAUTICAL JOURNAL , vol.122, no.1258, pp.1884-1915, 2018 (SCI-Expanded, Scopus) Sustainable Development

5. Aerothermodynamic shape optimization of hypersonic blunt bodies

ENGINEERING OPTIMIZATION , vol.47, no.7, pp.909-926, 2015 (SCI-Expanded, Scopus)

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

Havacılık ve Uzay Teknolojileri Dergisi , vol.7, pp.71-77, 2014 (TRDizin)

7. Convergence Error and Higher-Order Sensitivity Estimations

Eyi S.

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

8. Design optimization of rocket nozzles in chemically reacting flows

Yumusak M., EYİ S.

COMPUTERS & FLUIDS , vol.65, pp.25-34, 2012 (SCI-Expanded, Scopus)

9. 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, Scopus)

10. 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, Scopus)

11. Inverse airfoil design using the Navier Stokes equations

Eyi S., Lee K.

ENGINEERING OPTIMIZATION , vol.28, no.4, pp.245-262, 1997 (SCI-Expanded, Scopus)

12. 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, Scopus)

13. 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, Scopus)

14. 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, Scopus)

15. TRANSONIC AIRFOIL DESIGN BY CONSTRAINED OPTIMIZATION

LEE K., EYI S.

JOURNAL OF AIRCRAFT , vol.30, no.6, pp.805-806, 1993 (SCI-Expanded, Scopus)

16. AERODYNAMIC DESIGN VIA OPTIMIZATION

LEE K., EYI S.

JOURNAL OF AIRCRAFT , vol.29, no.6, pp.1012-1019, 1992 (SCI-Expanded, Scopus)

Papers Presented at Peer-Reviewed Scientific Conferences 76

1. 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, (Full Text)

2. 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, (Full Text)

3. 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, (Full Text)

4. 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, (Full Text)

5. 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, (Full Text)

6. 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, (Full Text)

7. 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, (Full Text)

8. 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, (Full Text)

9. 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, (Full Text)

10. 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)

11. 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, (Full Text)

12. 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, (Full Text)

13. 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, (Full Text)

14. 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, (Full Text)

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

2018 Fluid Dynamics Conference, Atlanta, Georgia, 25 - 29 June 2018, vol.2018, (Full Text)

16. 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, (Full Text)

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

2018 Fluid Dynamics Conference, Atlanta, Georgia, 25 - 29 June 2018, vol.2018, (Full Text)

18. 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, (Full Text)

19. 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, (Full Text)

20. Diffusion Models Implementation in Hypersonic Flow Regimes

9th Ankara International Aerospace Conference, 20 - 22 September 2017, vol.2017, (Full Text)

21. 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, (Full Text)

22. 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, (Full Text)

23. 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, (Full Text)

24. 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, (Full Text)

25. 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, (Full Text)

26. 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, (Full Text)

27. Three Dimensional Design Optimization Using Adjoint Method

Yıldırım A., EYİ S.

34th AIAA Applied Aerodynamics Conference, Washington, Kiribati, 13 - 17 June 2016, vol.2016, (Full Text)

28. Convergence Acceleration Based on Eigenvalue Analysis

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

29. 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)

30. Implicit Solution of One-Dimensional Transient Ablation

13th International Energy Conversion Engineering Conference, Orlando, FL, 27 July 2105 - 29 July 2015, vol.2015, (Full Text)

31. 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, (Full Text)

32. Diffusion Effect on Hypersonic Flow Using Fick’s Law

13th International Energy Conversion Engineering Conference, Orlando, FL, 27 - 20 July 2015, vol.2015, (Full Text)

33. 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, (Full Text)

34. 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)

35. 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, (Full Text)

36. Convergence Acceleration Using Convergence Error Estimation

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

37. 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, (Full Text)

38. 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, (Full Text)

39. 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, (Full Text)

40. 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)

41. 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, (Full Text)

42. 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, (Full Text)

43. 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, (Full Text)

44. 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, (Full Text)

45. 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, (Full Text)

46. 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, (Full Text)

47. Aerothermodynamic design optimization in hypersonic flows

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

48. 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, (Full Text)

49. Aerothermodynamic Shape Optimization ofHypersonic Blunt Bodies

Yumusak M., EYİ S.

21st AIAA ComputationalFluid Dynamics Conference, 24 - 27 June 2013, vol.2013, (Full Text)

50. Convergence acceleration based on convergence error estimation

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

51. 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, (Full Text)

52. 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, (Full Text)

53. 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)

54. 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, (Full Text)

55. 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, (Full Text)

56. 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, (Full Text)

57. Finite-Difference Sensitivity Calculation in Iteratively Solved Problems