Prof. Dr. SİNAN EYİ

AERONAUTICAL JOURNAL , cilt.122, sa.1258, ss.1884-1915, 2018 (SCI-Expanded, Scopus) Sürdürülebilir Kalkınma

5. Aerothermodynamic shape optimization of hypersonic blunt bodies

ENGINEERING OPTIMIZATION , cilt.47, sa.7, ss.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 , cilt.7, ss.71-77, 2014 (TRDizin)

7. Convergence Error and Higher-Order Sensitivity Estimations

Eyi S.

AIAA JOURNAL , cilt.50, sa.10, ss.2219-2234, 2012 (SCI-Expanded, Scopus)

8. Design optimization of rocket nozzles in chemically reacting flows

Yumusak M., EYİ S.

COMPUTERS & FLUIDS , cilt.65, ss.25-34, 2012 (SCI-Expanded, Scopus)

9. Effects of sensitivity derivatives on aerodynamic design optimization

Eyi S.

Inverse Problems In Science And Engineering , cilt.2, sa.1996, ss.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 , cilt.49, sa.2, ss.211-231, 2005 (SCI-Expanded, Scopus)

11. Inverse airfoil design using the Navier Stokes equations

ENGINEERING OPTIMIZATION , cilt.28, sa.4, ss.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 , cilt.33, sa.3, ss.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 , cilt.83, sa.3, ss.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 , cilt.31, sa.5, ss.1143-1147, 1994 (SCI-Expanded, Scopus)

15. TRANSONIC AIRFOIL DESIGN BY CONSTRAINED OPTIMIZATION

LEE K., EYI S.

JOURNAL OF AIRCRAFT , cilt.30, sa.6, ss.805-806, 1993 (SCI-Expanded, Scopus)

16. AERODYNAMIC DESIGN VIA OPTIMIZATION

LEE K., EYI S.

JOURNAL OF AIRCRAFT , cilt.29, sa.6, ss.1012-1019, 1992 (SCI-Expanded, Scopus)

Hakemli Bilimsel Toplantılarda Yayımlanmış Bildiriler 76

1. FIRLATMA RAMPALARINDA ATEŞLEME AŞIRI BASINÇ DALGALARININ HAD ANALİZİ

Duru M. Ö., Eyi S.

10. ULUSAL HAVACILIK ve UZAY KONFERANSI, Ankara, Türkiye, 18 - 20 Eylül 2024, ss.1-10, (Tam Metin Bildiri)

2. BEŞİNCİ NESİL BİR SAVAŞ UÇAĞININ KAVRAMSAL TASARIMI: UÇUŞ MEKANİĞİ YAKLAŞIMI

Kırkar A., Eyi S.

10. ULUSAL HAVACILIK ve UZAY KONFERANSI, Ankara, Türkiye, 18 - 20 Eylül 2024, ss.1-11, (Tam Metin Bildiri)

3. ROKET KALKIŞ RAMPALARINDA EĞİM AÇISININ VE GEOMETRİNİN ETKİSİNİN İNCELENMESİ

Yahya L., Soylu Z. S., Eyi S.

10. ULUSAL HAVACILIK ve UZAY KONFERANSI, Ankara, Türkiye, 18 - 20 Eylül 2024, ss.1-11, (Tam Metin Bildiri)

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, Japonya, 14 - 19 Temmuz 2024, sa.6, ss.1-22, (Tam Metin Bildiri)

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, İngiltere, 24 - 28 Haziran 2024, cilt.13, (Tam Metin Bildiri)

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, Almanya, 19 - 23 Haziran 2022, ss.1-6, (Tam Metin Bildiri)

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 Ağustos 2020, ss.1-10, (Tam Metin Bildiri)

8. 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, (Tam Metin Bildiri)

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, Türkiye, 18 - 20 Eylül 2019, cilt.10, (Tam Metin Bildiri)

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 Ocak 2019, cilt.2019, (Tam Metin Bildiri)

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

Akar G., EYİ S.

VII. Ulusal Havacılık Ve Uzay Konferansı, Türkiye, 12 - 14 Eylül 2018, cilt.2018, (Tam Metin Bildiri)

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 Temmuz 2018, cilt.10, (Tam Metin Bildiri)

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 Haziran 2018, cilt.2018, (Tam Metin Bildiri)

14. Aerothermodynamic Shape Optimization of Reentry Capsule

Kutkan H., EYİ S.

2018 Joint Thermophysics and Heat Transfer Conference, Atlanta, Georgia, 25 - 29 Haziran 2018, cilt.2018, (Tam Metin Bildiri)

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

2018 Fluid Dynamics Conference, Atlanta, Georgia, 25 - 29 Haziran 2018, cilt.2018, (Tam Metin Bildiri)

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 Haziran 2018, cilt.2018, (Tam Metin Bildiri)

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 Haziran 2018, cilt.2018, (Tam Metin Bildiri)

18. 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, (Tam Metin Bildiri)

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, Amerika Birleşik Devletleri, 8 - 12 Ocak 2018, (Tam Metin Bildiri)

20. Diffusion Models Implementation in Hypersonic Flow Regimes

9th Ankara International Aerospace Conference, 20 - 22 Eylül 2017, cilt.2017, (Tam Metin Bildiri)

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, Amerika Birleşik Devletleri, 5 - 09 Haziran 2017, (Tam Metin Bildiri)

22. Aerodynamic optimization of wing-body configuration using discrete adjoint method

YILDIRIM A., EYİ S.

35th AIAA Applied Aerodynamics Conference, 2017, Colorado, Amerika Birleşik Devletleri, 5 - 09 Haziran 2017, (Tam Metin Bildiri)

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 Temmuz 2016, cilt.2016, (Tam Metin Bildiri)

24. 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, (Tam Metin Bildiri)

25. 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, (Tam Metin Bildiri)

26. 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, (Tam Metin Bildiri)

27. Three Dimensional Design Optimization Using Adjoint Method

Yıldırım A., EYİ S.

34th AIAA Applied Aerodynamics Conference, Washington, Kiribati, 13 - 17 Haziran 2016, cilt.2016, (Tam Metin Bildiri)

28. Convergence Acceleration Based on Eigenvalue Analysis

46th AIAA Fluid Dynamics Conference, Washington, Kiribati, 13 - 17 Haziran 2016, cilt.2016, (Tam Metin Bildiri)

29. Modelling Thermochemical Nonequilibrium during Atmospheric Re-Entry

Pişkin T., EYİ S.

51st AIAA/SAE/ASEE Joint Propulsion Conference, Orlando, FL, 27 Ağustos - 27 Eylül 2015, cilt.2015, (Tam Metin Bildiri)

30. Implicit Solution of One-Dimensional Transient Ablation

13th International Energy Conversion Engineering Conference, Orlando, FL, 27 Temmuz 2105 - 29 Temmuz 2015, cilt.2015, (Tam Metin Bildiri)

31. 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, (Tam Metin Bildiri)

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

13th International Energy Conversion Engineering Conference, Orlando, FL, 27 - 20 Temmuz 2015, cilt.2015, (Tam Metin Bildiri)

33. 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, (Tam Metin Bildiri)

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 Haziran 2015, cilt.2015, (Tam Metin Bildiri)

35. 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, (Tam Metin Bildiri)

36. Convergence Acceleration Using Convergence Error Estimation

22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, 22 - 26 Haziran 2015, cilt.2015, (Tam Metin Bildiri)

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 Haziran 2105 - 26 Mayıs 2016, cilt.2015, (Tam Metin Bildiri)

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 Haziran 2015, (Tam Metin Bildiri)

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, Amerika Birleşik Devletleri, 16 - 20 Haziran 2014, cilt.2014, (Tam Metin Bildiri)

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, Amerika Birleşik Devletleri, 28 - 30 Temmuz 2014, (Tam Metin Bildiri)

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, Amerika Birleşik Devletleri, 28 - 30 Temmuz 2014, (Tam Metin Bildiri)

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, Amerika Birleşik Devletleri, 16 - 20 Haziran 2014, (Tam Metin Bildiri)

43. 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, (Tam Metin Bildiri)

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, Amerika Birleşik Devletleri, 28 - 30 Temmuz 2014, (Tam Metin Bildiri)

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, Amerika Birleşik Devletleri, 16 - 20 Haziran 2014, (Tam Metin Bildiri)

46. 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, (Tam Metin Bildiri)

47. Aerothermodynamic design optimization in hypersonic flows

49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, San Jose, CA, Amerika Birleşik Devletleri, 14 - 17 Temmuz 2013, (Tam Metin Bildiri)

48. 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, (Tam Metin Bildiri)

49. Aerothermodynamic Shape Optimization ofHypersonic Blunt Bodies

Yumusak M., EYİ S.

21st AIAA ComputationalFluid Dynamics Conference, 24 - 27 Haziran 2013, cilt.2013, (Tam Metin Bildiri)

50. Convergence acceleration based on convergence error estimation

21st AIAA Computational Fluid Dynamics Conference, San Diego, CA, Amerika Birleşik Devletleri, 24 - 27 Haziran 2013, (Tam Metin Bildiri)

51. Aerothermodynamic design optimization in hypersonic flows

49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, JPC 2013, California, Amerika Birleşik Devletleri, 14 - 17 Temmuz 2013, (Tam Metin Bildiri)

52. 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, (Tam Metin Bildiri)

53. Design optimization in hypersonic flows

EYİ S., Yumuşak M.

18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, Fransa, 24 - 28 Eylül 2012, (Tam Metin Bildiri)

54. 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, (Tam Metin Bildiri)

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, Amerika Birleşik Devletleri, 27 - 30 Haziran 2011, (Tam Metin Bildiri)

56. Design optimization in chemically reacting flows

Yumuşak M., EYİ S.

20th AIAA Computational Fluid Dynamics Conference 2011, Honolulu, HI, Amerika Birleşik Devletleri, 27 - 30 Haziran 2011, (Tam Metin Bildiri)

57. Finite-Difference Sensitivity Calculation in Iteratively Solved Problems

20th AIAA Computational Fluid Dynamics Conference 2011, Honolulu, HI, Amerika Birleşik Devletleri, 27 - 30 Haziran 2011, (Tam Metin Bildiri)

58. 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, Rusya, 12 - 16 Temmuz 2010, ss.241-246, (Tam Metin Bildiri)

59. Design Optimization in Non-equilibrium Reacting Flows

EYİ S., Ezertas A., Yumusak M.

6th International Conference on Computational Fluid Dynamics (ICCFD), St Petersburg, Rusya, 12 - 16 Temmuz 2010, ss.247-248, (Tam Metin Bildiri)

60. Performances of Numerical and Analytical Jacobians in Flow and Sensitivity Analysis

Ezertaş A. A., EYİ S.

19th AIAA Computational Fluid Dynamics, San-Antonio, Kuzey Mariana Adaları, 22 - 25 Haziran 2009, cilt.2009, (Tam Metin Bildiri)

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

Onur O., EYİ S.

17th AIAA Computational Fluid Dynamics Conference, Toronto, Kanada, 6 - 09 Haziran 2005, (Tam Metin Bildiri)

62. Inverse design of compressor cascades on parallel computers

Özhamam M., EYİ S.

40th AIAA Aerospace Sciences Meeting and Exhibit 2002, Reno, NV, Amerika Birleşik Devletleri, 14 - 17 Ocak 2002, (Tam Metin Bildiri)

63. Inverse design of compressor cascades

Kaplan B., EYİ S.

39th Aerospace Sciences Meeting and Exhibit 2001, Reno, NV, Amerika Birleşik Devletleri, 8 - 11 Ocak 2001, (Tam Metin Bildiri)

64. Aerodynamic sensitivity analysis in inverse design

Kocabiçak E., EYİ S.

8th Symposium on Multidisciplinary Analysis and Optimization 2000, Long Beach, CA, Amerika Birleşik Devletleri, 6 - 08 Eylül 2000, (Tam Metin Bildiri)

65. Effects of sensitivity analysis on turbomachinery blade design

Kocabiçak E., EYİ S.

35th Intersociety Energy Conversion Engineering Conference and Exhibit 2000, Las Vegas, NV, Amerika Birleşik Devletleri, 24 - 28 Temmuz 2000, (Tam Metin Bildiri)

66. Turbomachinery blade design via optimization

EYİ S., Lee K.

38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, Amerika Birleşik Devletleri, 10 - 13 Ocak 2000, (Tam Metin Bildiri)

67. Effects of sensitivity analysis on airfoil design

EYİ S., Lee K.

36th AIAA Aerospace Sciences Meeting and Exhibit, 1998, Nevada, Amerika Birleşik Devletleri, 12 - 15 Ocak 1998, (Tam Metin Bildiri)

68. Transonic turbomachinery blade design using optimization

EYİ S., Lee K.

35th Aerospace Sciences Meeting and Exhibit, 1997, Nevada, Amerika Birleşik Devletleri, 6 - 09 Ocak 1997, (Tam Metin Bildiri)

69. 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, Amerika Birleşik Devletleri, 17 - 20 Haziran 1996, ss.1-11, (Tam Metin Bildiri)

70. 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, (Tam Metin Bildiri)

71. 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, (Tam Metin Bildiri)

72. 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 Ocak 1995, cilt.1995, (Tam Metin Bildiri)

73. Inverse airfoil design using the Navier-stokes equations