Erim, Z., Yükselen, A. ve Kaynak, Ü. “Profillerin Teorik ve Deneysel İncelenmesi. Kısım I: Joukowski Profillerinin Sayısal Yöntemle İncelenmesi,” TÜBİTAK VII. Bilim Kongresi, Eylül 1980, İzmir, Türkiye.

Holst, T. L., Kaynak Ü., Gundy, K.L., Thomas S. D., Flores, J. and Chaderjian, N., “Numerical Solution of Transonic Wing Flows Using an Euler/Navier-Stokes Zonal Approach,’’ Journal of Aircraft, Vol. 24, No. 1, Ocak 1987, pp. 17-24.

Kaynak, Ü., Holst, T. L. and Cantwell, B. J., “Recent Improvements in Simulating Separated Wing Flows Using an Euler/Navier-Stokes Zonal Approach,” Open Forum Abstracts, AIAA Paper 85-1535, July 1985.

Holst, T. L., Thomas S. D., Kaynak Ü., Gundy, K.L.,  Flores, J. and Chaderjian, N.,  “Computational Aspects of Zonal Algorithms for Solving the Compressible Navier-Stokes Equations in Three Dimensions,” International Symposium on Computational Fluid Dynamics (ISCFD), Tokyo, Japan, Sept. 9-12, 1985.

“Computation of Transonic Separated Wing Flows Using an Euler/Navier-Stokes Zonal Approach,” PhD Thesis, Dept. of Aero. & Astro.,  Stanford University, Dec. 1985. (“Computation of Transonic Separated Wing Flows Using an Euler/Navier-Stokes Zonal Approach,” NASA TM-88311, July 1986).

Kaynak, Ü., Holst, T. L., Cantwell, B. J., and Sorenson, R. L., “Numerical Simulation of Transonic Separated Flows Over Low Aspect Ratio Wings,” Journal of Aircraft, Vol. 24, No. 8, Aug. 1987, pp. 531-539.

Flores, J. , Holst, T. L., Kaynak Ü., Gundy, K.L. and Thomas S. D., “Transonic Navier-Stokes Wing Solution Using a Zonal Approach: Part 1. Solution Methodology and Code Validation,” AGARD Paper 30A, 58th FDP Symposium on “Applications of Computational Fluid Dynamics in Aeronautics,” April 1986.

Kaynak, Ü. and Flores, J. “Advances in the Computation of Transonic Separated Flows Over Finite Wings,” Computers and Fluids Vol. 17, No. 2, pp. 313-332, 1989.

Kavsaoğlu, M. Ş., Kaynak, Ü. and Van Dalsem, W. R., “Three-Dimensional Application of the Johnson-King Turbulence Model for a Boundary-Layer Direct Method,” 3rd International Symposium on Computational Fluid Dynamics (ISCFD), Nagoya, Japan, Aug. 1989.

Kaynak, Ü., “Past, Present and Future of Computational Fluid Dynamics: Impact of Supercomputers,” Bulletin of the Technical University of İstanbul, Vol. 42, No. 4, 1989, pp. 429-452.

Kaynak, Ü. “Computational Turbulence Studies in Turkey,” AGARD TSR (Technical Status Review) on the “Appraisal of Turbulence Models in Flow Calculations,” April 1990, Friedrichshafen, Germany.

Dindar, M., Kaynak, Ü. and Fujii, K., “Nonequilibrium Turbulence Modeling Studies on Light Dynamic Stall of a NACA 0012 Airfoil,” Journal of Aircraft, Vol. 30, No. 3,  May-June 1993, pp. 304-308.

Kaynak, Ü., Tu, E., Dindar, M, and Fujii, K., “Nonequilibrium Turbulence Modeling Effects on Transonic Vortical Flows About Delta Wings”, AGARD FDP Symposium on Vortex Flow Aerodynamics, Oct. 1990, Scheveningen, Netherlands.

Kaynak, Ü., “Turbulence Modeling of Applied Computational Aerodynamics”, 4th. International Symposium on Computational Fluid Dynamics (ISCFD),  Sept. 9-12, 1991, Davis, CA, U.S.A.

Holst, T.L., Flores, J., Kaynak, Ü. and Chaderjian, N., “Navier-Stokes Computations About Complex Configurations Including a Complete F-16 Aircraft”, Applied Computational Aerodynamics, Progress Series in Astronautics and Aeronautics, AIAA Inc., Vol. 125, Washington DC, U.S.A.

Dindar, M. and Kaynak, Ü., “Effect of Turbulence Modeling on Dynamic Stall of a NACA0012 Airfoil”, AIAA Paper 92-0027, Jan. 1992, Reno, NV U.S.A.

Korkem B., Kaynak Ü., Yağcı H., “Prediction of Drag for a Class of Supercritical Airfoils”, Proceedings of European Forum on Recent Developments on Applications in Aeronautical CFD, Bristol, England, 1993.

Kaynak Ü., Dindar M., Yağcı H., Korkem B., “Transonic Vortex-Boundary Layer Interactions Around Swept Wings”, EuroMECH Colloquium 300, İstanbul, Turkey,  Sept. 27-30, 1993.

Cantekin, E., Kaynak, Ü.,  Dindar, M., “Impact of Artificial Dissipation Models on Boundary Layer Vorticity Fields”, EuroMECH Colloquium 300, İstanbul, Turkey, Sept. 27-30, 1993.

Dindar, M. ve Kaynak, Ü. “Effect of Turbulence Modeling on Dynamic Stall Computations” AGARD 75th FDP Symposium on Aerodynamics and Aeroacoustics of Rotorcraft,  10-14 October 1994, Berlin, Germany.

Altan, B. ve Kaynak, Ü. “Türkiye’de Havacılık ve Uzay Sanayiinin Gelişimi ve Geleceğe Bakış,” TSKGV “MSB ve Türk Savunma Sanayii İlişkileri Paneli, 31.05.1994, TÜBİTAK, Ankara.

Kaynak, Ü. “İnsansız Hava Araçları (İHA) Teknolojisi ve TAI İnsansız Hava Aracı Programı,” Birinci Havacılık Sempozyumu, Hava Harp Okulu, 9-10 Haz. 1994, İstanbul.

Kaynak, Ü., ‘Turkish Unmanned Air Vehicle Developments’, AGARD CP 591, ‘Subsystem Integration for Tactical Missiles and Design and Operation of Unmanned Air Vehicles (DOUAV), November 1996.

Kaynak, Ü, Yılmaz, Ş. And Çete, R., ‘Accuracy Improvements for Transonic Wing Flows Using a Nonequilibrium Algebraic Turbulence Model’, 1998 World Aviation Congress, Paper No. 985573, Sep. 1998, Anaheim, California.

Doğrusöz, Ş., Kavsaoğlu, M. Ş., Kaynak, Ü, ‘Numerical Solution of Hypersonic Compression Corner Flows’, 2001, AIAA Paper No: 2001-1750

Yıllıkçı, Y.K., Kaynak, Ü.,  Solakoğlu, E. ‘Airbus A400M Projesinde Tasarım ve Geliştirme Yaklaşımları’, SAVTEK Savunma Teknolojileri Kongresi, 24-25 Ekim 2002, Ankara.

Aziz, Ş., Kavsaoğlu, M. Ş., ve Kaynak, Ü, ‘Numerical Analysis of Shock Wave Laminar Boundary Layer Interactions in Hypersonic High Temperature Flows over Compression Corners’, International Conference on High-Speed Flow Fundamental Problems, 21-24 September 2004, Zhukowsky, Russia. 

Durmuş, G., Kavsaoğlu, M. Ş., ve Kaynak, Ü.,’Parallel Solution of Low Aspect Ratio Rectangular Flat Wings in Compressible Flow’, AIAA Paper No: 2005-1224, Jan. 2005, Reno, NV U.S.A.

Aziz, Ş., Kavsaoğlu, M. Ş., Kaynak, Ü.,’Effects of Wall to Stagnation Temperature Ratio on Hypersonic Corner Flows’, AIAA Paper No: 2005-5141, June 2005, Toronto, Ontario, Kanada

Kaynak, Ü., “Havacılık Sanayi Program Yönetiminde Kullanılan Modern Yönetim Araçları ve Görsel Yöntemler”, 1. Proje Yönetim Sempozyumu, TOBB-ETÜ, 19 Kasım 2005.

Bayraktar, H., Bayraktar, S., Kaynak, Ü., “Bayraktar Mini İnsansız Hava Aracının Tasarım Özellikleri ve Uçuş Performansı”, HaSem’06, Kayseri VI. Havacılık Sempozyumu, 12-14 Mayıs 2006, Nevşehir.

Gürdamar, E., Çete, R., Aksel, H., Kaynak, Ü., “İki-Denklemli Türbülans Modelleri İle Transonik Akış Hesaplamaları”, HaSem’06, Kayseri VI. Havacılık Sempozyumu, 12-14 Mayıs 2006, Nevşehir.

Gürdamar, E., Çete, R., Aksel, H. and Kaynak, Ü., “Kanatlar Üzerinde Transonik Akışkanların İki-Denklemli Türbülans Modelleriyle Çözümü”, SAVTEK 2006, Savunma Teknolojileri Kongresi, 29-30 Haziran 2006, ODTÜ, Ankara.

Çete, R. and Kaynak, Ü, “A New Approximate Factorization Method Suitable for Structured and Unstructured Grids”, AIAA-2006-3789, 9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, June 05-08, 2006, San Francisco , CA, USA.

Gürdamar, E., Çete, R., Aksel, H. and Kaynak, Ü., “Determination of Transition Correlations For Zero-Pressure Gradient Flat Plate Flows”, AIAA-2006-3170, 24th AIAA Applied Aerodynamics Conference, June 05-08, 2006, San Francisco , CA, USA.

Durmuş, G., Kavsaoğlu, M., and Kaynak, Ü., “Unsteady Navier Stokes Solutions of Low Aspect Ratio Rectangular Wings in Compressible Flow, ParCFD-2007-065, International Conference on Parallel Computational Fluid Dynamics, May 21-24 2007, Antalya.

Kaynak, Ü. and Gürdamar, E. “Prediction of Transition Using Correlation Based  Engineering Transition Model”, AIAC-2007-053, 4^th Ankara International Aerospace Conference, Ankara.

Kaynak, Ü. ve Gümüş, B., “Savunma Sanayiine Yönelik İnsan Kaynakları Eğitimi”, II. Proje Yönetimi Sempozyumu: SAVUNMA SANAYİİNDE KOBİLER”, II. Proje Yönetimi Sempozyumu, 8 Aralık 2007, Ankara.

Kaynak, Ü. and Gürdamar, E. “Boundary-Layer Transition Under the Effects of Compressibility and Roughness for the Correlation Based Transition Model”, AIAA Aerospace Sciences Meeting, 07-10 January, 2008, Reno, Nevada, ABD.

Çete, A.R., Yükselen, M.A. and Kaynak, Ü. “A Unifying Grid Approach for Solving Potential Flows Applicable to Structured and Unstructured Grid Configurations” Computers and Fluids, 37 (2008) 35-50.

M. Serdar Genç, Gary D. Lock, Ünver KAYNAK, "An Experimental and Computational Study of Low Re Number Transitional Flows over an Aerofoil with Leading Edge Slat", AIAA-2008-8877, 8th AIAA Aviation Technology, Integration and Operations Conference (ATIO 2008), Anchorage, Alaska, USA, 14-19 September 2008.

M. Serdar Genç, Ünver KAYNAK "Kanat Profili Etrafındaki Düşük Reynolds Sayılı Akım Kontrolü ve Türbülansa Geçiş Modellerinin Etkisi", ANOVA Kullanıcılar Konferansı 2, Ankara, Türkiye, 7-9 Ekim 2008.

M. Serdar Genç, Ünver KAYNAK, Gary D. Lock, "Hücum Kenarı Slatlı Kanat Profili Etrafındaki Düşük Re Sayılı Geçiş Akışında Akım Ayrılmasının Kontrolü" II. Ulusal Havacılık ve Uzay Konferansı, UHUK 2008, İTÜ, İstanbul, Türkiye, 15-17 Ekim 2008.

M. Serdar Genç, Ünver Kaynak, “Control of Flow Separation and Transition Point over an Aerofoil at Low Re Number using Blowing”, AIAA 19th AIAA Computational Fluid Dynamics, 22 - 25 Jun 2009, Grand Hyatt Hotel, San Antonio, Texas, USA.

M. Serdar Genç, Ünver Kaynak, “Control of Laminar Separation over an NACA2415 Aerofoil at Low Re Transitional Flow using Blowing/Suction”, 13th International Conference on AEROSPACE SCIENCES & AVIATION TECHNOLOGY, May 26 – 28, 2009, ASAT 2009 – Military Technical College, Cairo, EGYPT.

M. Serdar Genç, Ünver Kaynak, Nafiz Kahraman, “Control of Flow Separation and Transition Point over an Aerofoil at Low Re Number using Suction”, 17. Ulusal Isı Bilimi ve Tekniği Kongresi, ULIBTK’09, Sivas, Türkiye, 24-27 Haziran 2009.

M. Serdar Genç, Ünver Kaynak, Gary D. Lock, "Flow over an Aerofoil without and with Leading Edge Slat at a Transitional Reynolds Number", Proc IMechE, Part G- Journal of Aerospace Engineering.