Prof. Dr. ÜNVER KAYNAK

SCI, SSCI ve AHCI İndekslerine Giren Dergilerde Yayınlanan Makaleler

A correlation-based algebraic transition model

Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science , cilt.232, sa.21, ss.3915-3929, 2018 (SCI-Expanded)

A Novel Alternating Cell Directions Implicit Method for the solution of incompressible navier stokes equations on unstructured grids

Baş O., Cete A., Mengi S., TUNCER İ. H., Kaynak Ü.

Journal of Applied Fluid Mechanics , cilt.10, sa.6, ss.1561-1570, 2017 (SCI-Expanded)

A Mach-uniform preconditioner for incompressible and subsonic flows

Baş O., TUNCER İ. H., Kaynak Ü.

International Journal for Numerical Methods in Fluids , cilt.74, sa.2, ss.100-112, 2014 (SCI-Expanded)

Unsteady compressible flow simulation around low-aspect-ratio rectangular flat wings

Durmuş G., Kavsaoǧlu M., Kaynak Ü.

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering , cilt.225, sa.6, ss.675-687, 2011 (SCI-Expanded)

Performance of transition model for predicting low Re aerofoil flows without/with single and simultaneous blowing and suction

GENÇ M. S., Kaynak Ü., YAPICI H.

European Journal of Mechanics, B/Fluids , cilt.30, sa.2, ss.218-235, 2011 (SCI-Expanded)

Flow over an aerofoil without and with a leading-edge slat at a transitional Reynolds number

GENÇ M. S., Kaynak Ü., Lock G.

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering , cilt.223, sa.3, ss.217-231, 2009 (SCI-Expanded)

A unifying grid approach for solving potential flows applicable to structured and unstructured grid configurations

Çete A. R., Yükselen M. A., Kaynak Ü.

Computers and Fluids , cilt.37, sa.1, ss.35-50, 2008 (SCI-Expanded)

Diğer Dergilerde Yayınlanan Makaleler

Longitudinal Stability Analysis of a UAV under the Uncertainty of Two Stability Derivatives

ÖZDEMİR U., KAVSAOĞLU M. Ş., ÖZNALBANT Z., KAYNAK Ü.

Anadolu University Journal of Science and Technology-A Applied Sciences and Engineering , ss.278-290, 2018 (Hakemli Dergi)

Design of a flight stabilizer system and automatic control using HIL test platform

Akyürek Ş., Özden G. S., Atlas E., Kasnakoğlu C., Kaynak Ü.

International Journal of Mechanical Engineering and Robotics Research , cilt.5, sa.1, ss.77-81, 2016 (Scopus)

Control Loss Recovery Autopilot Design for Fixed-Wing Aircraft

Akyürek Ş., Kürkçü B., Kaynak Ü., Kasnakoğlu C.

IFAC-PapersOnLine , cilt.49, sa.9, ss.117-123, 2016 (Scopus)

Altitude Control for Small Fixed-Wing Aircraft Using H∞ Loop-Shaping Method

Akyurek S., Kaynak Ü., Kasnakoglu C.

IFAC-PapersOnLine , cilt.49, sa.9, ss.111-116, 2016 (Scopus)

Nonequilibrium turbulence modeling study on light dynamic stall of a NACA0012 airfoil

Dindar M., Kaynak Ü., Fujii K.

Journal of Aircraft , cilt.30, sa.3, ss.304-308, 1993 (Scopus)

Three-dimensional application of the Johnson-King turbulence model for a boundary-layer direct method

Kavsaoǧlu M. Ş., Kaynak Ü., Van Dalsem W. R.

Computers and Fluids , cilt.19, sa.3-4, ss.363-376, 1991 (Scopus)

Advances in the computation of transonic separated flows over finite wings

Kaynak Ü., Flores J.

Computers and Fluids , cilt.17, sa.2, ss.313-332, 1989 (Scopus)

Transonic wing flows using an Euler/Navier-Stokes zonal approach

Holst T. L., Gundy K. L., Flores J., Chaderjian N. M., Kaynak Ü.

Journal of Aircraft , cilt.24, sa.1, ss.17-24, 1987 (Scopus)

Numerical simulation of transonic separated flows over low-aspect-ratio wings

Kaynak Ü., Holst T. L., Cantwell B. J., Sorenson R. L.

Journal of Aircraft , cilt.24, sa.8, ss.531-539, 1987 (Scopus)

Hakemli Bilimsel Toplantılarda Yayımlanmış Bildiriler

A revised one-equation transitional model for external aerodynamics

Çakmakçıoğlu S. Ç., Baş O., Mura R., KAYNAK Ü.

AIAA AVIATION 2020 FORUM, Virtual, Online, 15 - 19 Haziran 2020, cilt.1 PartF, (Tam Metin Bildiri)

Output feedback sliding mode control of a fixed-wing UAV under rudder loss

Gunes U., Sel A., Kasnakoglu C., Kaynak Ü.

AIAA Scitech Forum, 2019, California, Amerika Birleşik Devletleri, 7 - 11 Ocak 2019, (Tam Metin Bildiri)

Rudder loss recovery autopilot system for a small fixed-wing aircraft

Akyurek S., Gunes U., Elbir O., Kasnakoglu C., Kaynak Ü.

10th International Conference on Electrical and Electronics Engineering, ELECO 2017, Bursa, Türkiye, 29 Kasım - 02 Aralık 2017, cilt.2018-January, ss.752-757, (Tam Metin Bildiri)

Heading Hold Autopilot Design for Fixed Wing Aircraft

Akyürek Ş., KASNAKOĞLU C., KAYNAK Ü.

AIAA Guidance, Navigation, and Control Conference, AIAA SciTech Forum, 8 - 12 Ocak 2018, (Tam Metin Bildiri)

Design of a flight stabilizer for fixed-wing aircrafts using H∞ loop shaping method

Akyurek Ş., Ozden G. S., Kürkçü B., Kaynak Ü., Kasnakoǧlu C.

9th International Conference on Electrical and Electronics Engineering, ELECO 2015, Bursa, Türkiye, 26 - 28 Kasım 2015, ss.790-795, (Tam Metin Bildiri)

Drag analysis of a supersonic fighter aircraft

Akgun O., Golcuk A. I., KURTULUŞ D. F., Kaynak Ü.

9th International Conference on Computational Fluid Dynamics, ICCFD 2016, İstanbul, Türkiye, 11 - 15 Temmuz 2016, (Tam Metin Bildiri)

Aerodynamic analysis of flow characteristics over rotors using CFD methods

Öktem O., Başaran E., Kaynak Ü.

9th International Conference on Computational Fluid Dynamics, ICCFD 2016, İstanbul, Türkiye, 11 - 15 Temmuz 2016, (Tam Metin Bildiri)

Numerical investigation of winglets used to improve the flying performance of unmanned aerial vehicle

Kaynak Ü., Çoban A. B.

9th International Conference on Computational Fluid Dynamics, ICCFD 2016, İstanbul, Türkiye, 11 - 15 Temmuz 2016, (Tam Metin Bildiri)

Design study of a short-range airborne UAV radar for human monitoring

Gürbüz S. Z., Kaynak Ü., Özkan B., Kocaman O. C., Kiyici F., Tekeli B.

48th Asilomar Conference on Signals, Systems and Computers, ACSSC 2015, California, Amerika Birleşik Devletleri, 2 - 05 Kasım 2014, cilt.2015-April, ss.568-572, (Tam Metin Bildiri) Sürdürülebilir Kalkınma

Hardware-in-the-loop test platform for a small fixed wing unmanned aerial vehicle embedded controller

Ertin O. B., Korkmaz H., Kaynak Ü., Kasnakoglu C.

32nd IASTED International Conference on Modelling, Identification and Control, MIC 2013, Innsbruck, Avusturya, 11 - 13 Şubat 2013, ss.282-285, (Tam Metin Bildiri)

A novel intermittency distribution based transition model for low-re number airfoils

Baş O., Çakmakçioǧlu S. Ç., Kaynak Ü.

31st AIAA Applied Aerodynamics Conference, San Diego, CA, Amerika Birleşik Devletleri, 24 - 27 Haziran 2013, (Tam Metin Bildiri)

Design of a Flight Stabilizer System for a Small Fixed Wing Unmanned Aerial Vehicle using System Identification

Korkmaz H., Ertin O. B., Kasnakoǧlu C., Kaynak Ü.

1st IFAC Workshop on Advances in Control and Automation Theory for Transportation Applications, ACATTA 2013, İstanbul, Türkiye, 16 - 17 Eylül 2013, cilt.1, ss.145-149, (Tam Metin Bildiri)

Transition at low-re numbers for UAV type airfoils at high subsonic mach numbers

Çakmakçioǧlu S. Ç., Kaynak Ü., GENÇ M. S.

30th AIAA Applied Aerodynamics Conference 2012, New Orleans, LA, Amerika Birleşik Devletleri, 25 - 28 Haziran 2012, ss.1680-1697, (Tam Metin Bildiri)

Automatic recovery and autonomous navigation of disabled aircraft after control surface actuator jam

Kasnakoǧlu C., Kaynak Ü.

AIAA Guidance, Navigation, and Control Conference, Toronto, Kanada, 2 - 05 Ağustos 2010, (Tam Metin Bildiri)

Control of flow separation and transition point over an aerofoil at low Re number using simultaneous blowing and suction

GENÇ M. S., Kaynak Ü.

19th AIAA Computational Fluid Dynamics Conference, San Antonio, TX, Amerika Birleşik Devletleri, 22 - 25 Haziran 2009, (Tam Metin Bildiri)

Technology management in turkish defense industry

Gumus B., Demir V., Kaynak Ü.

PICMET 2009 - 2009 Portland International Conference on Management of Engineering and Technology, Portland, OR, Amerika Birleşik Devletleri, 2 - 06 Ağustos 2009, ss.2905-2912, (Tam Metin Bildiri)

Unsteady navier stokes solutions of low aspect ratio rectangular flat wings in compressible Flow

Durmuş G., Kavsaoǧlu M., Kaynak Ü.

Parallel Computational Fluid Dynamics, Parallel CFD 2007, Antalya, Türkiye, 21 - 24 Mayıs 2007, cilt.67 LNCSE, ss.297-304, (Tam Metin Bildiri)

Boundary-layer transition under the effect of compressibility for the correlation Based Transition Model

Kaynak Ü., Gürdamar E.

46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Amerika Birleşik Devletleri, 7 - 10 Ocak 2008, (Tam Metin Bildiri)

An experimental and computational study of low Re number transitional flows over an aerofoil with leading edge slat

GENÇ M. S., Lock G., Kaynak Ü.

8th AIAA Aviation Technology, Integration and Operations (ATIO) Conference, Anchorage, AK, Amerika Birleşik Devletleri, 14 - 19 Eylül 2008, (Tam Metin Bildiri)

A new approximate factorization method suitable for structured and unstructured grids

Çete R., Kaynak Ü.

9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference Proceedings, San Francisco, CA, Amerika Birleşik Devletleri, 5 - 08 Haziran 2006, cilt.4, ss.2462-2471, (Tam Metin Bildiri)

Determination of transition correlations for zero-pressure gradient flat plate flows

Gürdamar E., Çete R., Aksel H., Kaynak Ü.

24th AIAA Applied Aerodynamics Conference, San Francisco, CA, Amerika Birleşik Devletleri, 5 - 08 Haziran 2006, cilt.2, ss.987-994, (Tam Metin Bildiri)

Parallel solution of low aspect ratio rectangular flat wings in compressible flow

Durmuş G., Kavsaoǧlu M., Kaynak Ü.

43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Amerika Birleşik Devletleri, 10 - 13 Ocak 2005, ss.10697-10709, (Tam Metin Bildiri)

Effects of wall to stagnation temperature ratio on hypersonic corner flows

Aziz Ş., Kavsaoǧlu M. Ş., Kaynak Ü.

35th AIAA Fluid Dynamics Conference and Exhibit, Toronto, Kanada, 6 - 09 Haziran 2005, (Tam Metin Bildiri)

Numerical solution of hypersonic compression corner flows

Doǧrusöz Ş., Kavsaoǧlu M. Ş., Kaynak Ü.

10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001, Kyoto, Japonya, 24 - 27 Nisan 2001, (Tam Metin Bildiri)