Prof. OKTAY ÖZCAN

Publication Network

Articles 27

1. Passive control of shock wave turbulent boundary layer interaction via a wall jet

Yolaçtı A., ÖZCAN O., Kaya K.

Journal of the Brazilian Society of Mechanical Sciences and Engineering , vol.48, no.3, 2026 (SCI-Expanded, Scopus)

2. Numerical calculations for the length of the transitory zone in partially filled circular pipes with steep slope

KAYA K., ÖZCAN O.

JOURNAL OF POLYTECHNIC-POLITEKNIK DERGISI , vol.28, no.6, pp.1865-1879, 2025 (ESCI, TRDizin)

3. Correlations Describing Laminar Hydrodynamic Development in a Circular Pipe

Kaya K., ÖZCAN O.

Journal of Fluids Engineering , vol.145, no.5, 2023 (SCI-Expanded, Scopus)

4. A NUMERICAL STUDY FOR COATING OF VENTILATION DUCTS USING JET INJECTION

Sezer C., Kaya K., Onal B. S., Heperkan H. A., ÖZCAN O.

Thermal Science , vol.27, no.5, pp.3769-3781, 2023 (SCI-Expanded, Scopus)

5. An approximate analytic solution of uniform laminar flow in a circular open channel

Kaya K., Özcan O.

Journal of the Brazilian Society of Mechanical Sciences and Engineering , vol.43, no.6, 2021 (SCI-Expanded, Scopus)

6. A numerical investigation on aerodynamic characteristics of an air-cushion vehicle

Kaya K., ÖZCAN O.

Journal of Wind Engineering and Industrial Aerodynamics , vol.120, pp.70-80, 2013 (SCI-Expanded, Scopus)

7. An experimental and numerical study of laminar natural convection in a differentially-heated cubical enclosure

KÜREKCİ N. A., ÖZCAN O.

Isi Bilimi Ve Teknigi Dergisi/ Journal of Thermal Science and Technology , vol.32, no.1, pp.1-8, 2012 (SCI-Expanded, Scopus, TRDizin)

8. A turbulent jet in crossflow analysed with proper orthogonal decomposition

Meyer K. E., Pedersen J. M., ̈Ozcan O.

Journal of Fluid Mechanics , vol.583, pp.199-227, 2007 (SCI-Expanded, Scopus)

9. A visual description of the convective flow field around the head of a human

ÖZCAN O., Meyer K., Melikov A.

Journal of Visualization , vol.8, no.1, pp.23-31, 2005 (SCI-Expanded, Scopus)

10. Measurement of mean rotation and strain-rate tensors by using stereoscopic PIV

ÖZCAN O., Meyer K., Larsen P.

Experiments in Fluids , vol.39, no.4, pp.771-783, 2005 (SCI-Expanded, Scopus)

11. Three-dimensional flow and turbulence structure in electrostatic precipitator by stereo PIV

Ullum T., Larsen P., ÖZCAN O.

Experiments in Fluids , vol.36, no.1, pp.91-99, 2004 (SCI-Expanded, Scopus)

12. Laser Doppler anemometry study of a turbulent jet in crossflow

ÖZCAN O., Larsen P. S.

AIAA Journal , vol.41, no.8, pp.1614-1616, 2003 (SCI-Expanded, Scopus)

13. Flow mapping of a jet in crossflow with stereoscopic PIV

Meyer K. E., Özcan O., Westergaard C. H.

Journal of Visualization , vol.5, no.3, pp.225-231, 2002 (Scopus)

14. Comment on “Wakes of three axisymmetric bodies at zero angle of attack”

Özcan O., Johnson D., Simpson R. L.

AIAA Journal , vol.33, no.3, pp.569-570, 1995 (Scopus)

15. Aerodynamic characteristics of external store configurations at low speeds

Özcan O., Üenal M., Aslan A. R., Bozkurt Y. E., Aydın N. G.

Journal of Aircraft , vol.32, no.1, pp.161-170, 1995 (Scopus)

16. Skin-friction measurements in three-dimensional, supersonic shock-wave/boundary-layer interaction

Wideman J. K., Brown J. L., Miles J. B., Özcan O.

AIAA Journal , vol.33, no.5, pp.805-811, 1995 (Scopus)

17. Reply by the Authors to G. Emanuel

Özcan O., Edis F. E., Aslan A. R., Pınar İ.

Journal of Aircraft , vol.32, no.5, 1995 (Scopus)

18. Inverse solutions of the Prandtl-Meyer function

Özcan O., Edis F. E., Aslan A. R., Pınar İ.

Journal of Aircraft , vol.31, no.6, pp.1422-1424, 1994 (Scopus)

19. Cylinder-induced shock-wave boundary-layer interaction

Özcan O., Yüceil K. B.

AIAA Journal , vol.30, no.4, pp.1130-1132, 1992 (Scopus)

20. Shock-wave/boundary-layer interaction at a swept compression corner

Özcan O., Kaya M. O.

AIAA Journal , vol.27, no.11, pp.1646-1648, 1989 (Scopus)

21. Three-component LDA measurements in a turbulent boundary layer

Özcan O.

Experiments in Fluids , vol.6, no.5, pp.327-334, 1988 (Scopus)

22. Measurements of turbulent flow behind a wing-body junction

Özcan O., Ölçmen M.

AIAA Journal , vol.26, no.4, pp.494-496, 1988 (Scopus)

23. MEASUREMENTS IN THE WAKE OF A WING-BODY JUNCTION.

Ozcan O., Olcmen M.

Bulletin of the Technical University of Istanbul , vol.40, no.3, pp.537-549, 1987 (Scopus)

24. Measurements in the wake of a wing-body junction.

Ozcan O., Olcmen S.

ISTANBUL TEK. BUL. , vol.40 , 1987, pp.537-549, 1987 (Scopus)

25. THREE-COMPONENT LDA SYSTEM FOR TURBULENCE AND MEAN VELOCITY MEASUREMENTS.

Ozcan O., Johnson D. A.

Bulletin of the Technical University of Istanbul , vol.38, no.4, pp.409-419, 1985 (Scopus)

26. A three-component LDA system for turbulence and mean velocity measurements.

Ozcan O., Johnson D.

ISTANBUL TEK. UNIV. BUL. , vol.38, no.4 , 1985, pp.409-419, 1985 (Scopus)

27. Supersonic separated flow past a cylindrical obstacle on a flat plate

Ozcan O., Holtt M.

AIAA Journal , vol.22, no.5, pp.611-617, 1984 (Scopus)

Papers Presented at Peer-Reviewed Scientific Conferences 5

1. Computational Investigation of Turbulent Shock Wave Boundary Layer Interaction via Secondary Recirculation Induced Wall Jet

Yolacti A., Kaya K., ÖZCAN O.

10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023, İstanbul, Turkey, 7 - 09 June 2023, (Full Text)

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