Doç. Dr. HARİKA SENEM KAHVECİ

Makaleler 12

1. Experimental investigation of momentum ratio and impingement angle effects on spray characteristics of triplet and pentad injectors

Gulmez S., Kahveci H. S.

International Journal of Multiphase Flow , cilt.177, 2024 (SCI-Expanded, Scopus)

2. Investigation of a rotor blade with tip cooling subject to a nonuniform temperature profile

Kahveci H. S.

Journal of Turbomachinery , cilt.143, sa.7, 2021 (SCI-Expanded, Scopus)

3. Effect of Turbine Blade Tip Cooling Configuration on Tip Leakage Flow and Heat Transfer

Sakaoglu S., Kahveci H. S.

JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME , cilt.142, sa.2, 2020 (SCI-Expanded, Scopus)

4. Effect of turbulence modeling for the prediction of flow and heat transfer in rotorcraft avionics bay

Akin A., Kahveci H. S.

AEROSPACE SCIENCE AND TECHNOLOGY , cilt.95, 2019 (SCI-Expanded, Scopus)

5. Effect of cavity depth on thermal performance of a cooled blade tip under rotation

Sakaoglu S., Kahveci H. S.

INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER , cilt.143, 2019 (SCI-Expanded, Scopus)

6. An optimization study for rotorcraft avionics bay cooling

Akin A., Kahveci H. S.

AEROSPACE SCIENCE AND TECHNOLOGY , cilt.90, ss.1-11, 2019 (SCI-Expanded, Scopus)

7. USE OF ARTIFICIAL NEURAL NETWORK IN ROTORCRAFT COOLING SYSTEM

Akin A., Kahveci H. S.

Havacılık ve Uzay Teknolojileri Dergisi , cilt.12, sa.2, ss.157-170, 2019 (TRDizin)

8. EFFECTS OF PIN FIN SHAPE AND SIZE ON TURBINE BLADE TRAILING EDGE FLOW AND HEAT TRANSFER

Tuncel T., Kahveci H. S.

ISI BILIMI VE TEKNIGI DERGISI-JOURNAL OF THERMAL SCIENCE AND TECHNOLOGY , cilt.39, sa.2, ss.191-207, 2019 (SCI-Expanded, Scopus, TRDizin)

9. Uncertainty Analysis of Heat Transfer Predictions Using Statistically Modeled Data From a Cooled 1-1/2 Stage High-Pressure Transonic Turbine

Kahveci H. S., Kırtley K.

JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME , cilt.136, 2014 (SCI-Expanded, Scopus)

10. Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine-Part II: Effect of Cooling Variation on the Vane Airfoil and Inner End Wall

Kahveci H. S., Haldeman C., Mathıson R., Dunn M.

JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME , cilt.135, 2013 (SCI-Expanded, Scopus)

11. Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine-Part I: Experimental Configuration and Data Review With Inlet Temperature Profile Effects

Kahveci H. S., Haldeman C., Mathıson R., Dunn M.

JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME , cilt.135, 2013 (SCI-Expanded, Scopus)

12. Validation of MISES Two-Dimensional Boundary Layer Code for High-Pressure Turbine Aerodynamic Design

Andrew P., Kahveci H. S.

JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME , cilt.131, 2009 (SCI-Expanded, Scopus)

Hakemli Bilimsel Toplantılarda Yayımlanmış Bildiriler 13

1. Data-Driven Optimization of Transition Modeling for Improved Boundary Layer Predictions

Peksag B. B., Kahveci H. S.

13th Ankara International Aerospace Conference (AIAC), Ankara, Türkiye, 17 - 19 Eylül 2025, ss.1-20, (Tam Metin Bildiri)

2. Computational Investigation of Perpendicular Blade-Vortex Interaction

Arican M., Kahveci H. S.

13th Ankara International Aerospace Conference (AIAC), Ankara, Türkiye, 17 - 19 Eylül 2025, ss.1-19, (Tam Metin Bildiri)

3. Estimating Sweet Spot for UAV Formation Flight Using Vortex Lattice Method and Machine Learning

Tatar U., Kahveci H. S.

12th Ankara International Aerospace Conference (AIAC), Online, 13 - 14 Eylül 2023, (Tam Metin Bildiri)

4. Numerical Simulation of Spray Characteristics of Doublet Injectors

Gulmez S., Kahveci H. S.

11th Ankara International Aerospace Conference (AIAC), Virtual, Online, 8 - 10 Eylül 2021, (Tam Metin Bildiri)

5. Investigation of a rotor blade with tip cooling subject to a nonuniform temperature profile

Kahveci H. S.

ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, GT 2020, Virtual, Online, 21 - 25 Eylül 2020, cilt.7B-2020, (Tam Metin Bildiri)

6. Gas Turbine Blade Cooling Technology, Advances, and Challenges

Kahveci H. S.

10th Ankara International Aerospace Conference, Ankara, Türkiye, 18 - 20 Eylül 2019, (Tam Metin Bildiri)

7. EFFECT OF TURBINE BLADE TIP COOLING CONFIGURATION ON TIP LEAKAGE FLOW AND HEAT TRANSFER

Sakaoğlu S., Kahveci H. S.

ASME Turbo Expo: Turbomachinery Technical Conference and Exposition, Arizona, Amerika Birleşik Devletleri, 17 - 21 Haziran 2019, (Tam Metin Bildiri)

8. Comparison of Temperature Profile and Heat Transfer Predictions With Statistically Modeled Data From a Cooled 1 1 2 Stage High Pressure Transonic Turbine

Kahveci H. S., Kırtley K.

ASME Turbo Expo 2013, Volume 3C: Heat Transfer, Texas, Amerika Birleşik Devletleri, 3 - 07 Haziran 2013, (Tam Metin Bildiri)

9. Heat Transfer for the Film Cooled Vane of a 1 1 2 Stage High Pressure Transonic Turbine Part I Experimental Configuration and Data Review With Inlet Temperature Profile Effects

Kahveci H. S., Haldeman C., Mathıson R., Dunn M.

ASME Turbo Expo 2011, Volume 5: Heat Transfer, Parts A and B, Vancouver, Kanada, 6 - 10 Haziran 2011, cilt.5, ss.1719-1733, (Tam Metin Bildiri)

10. Heat Transfer for the Film Cooled Vane of a 1 1 2 Stage High Pressure Transonic Turbine Part II Effect of Cooling Variation on the Vane Airfoil and Inner Endwall

Kahveci H. S., Haldeman C., Mathıson R., Dunn M.

ASME Turbo Expo 2011, Volume 5: Heat Transfer, Parts A and B, Vancouver, Kanada, 6 - 10 Haziran 2011, cilt.5, ss.1735-1744, (Tam Metin Bildiri)

Yayın

Yayın (WoS)

Yayın (Scopus)

Atıf (WoS)

116

H-İndeks (WoS)

Atıf (Scopus)

163

H-İndeks (Scopus)

Atıf (Scholar)

200

Doç. Dr. HARİKA SENEM KAHVECİ

Yayınlar & Eserler

1. Experimental investigation of momentum ratio and impingement angle effects on spray characteristics of triplet and pentad injectors

2. Investigation of a rotor blade with tip cooling subject to a nonuniform temperature profile

3. Effect of Turbine Blade Tip Cooling Configuration on Tip Leakage Flow and Heat Transfer

4. Effect of turbulence modeling for the prediction of flow and heat transfer in rotorcraft avionics bay

5. Effect of cavity depth on thermal performance of a cooled blade tip under rotation

6. An optimization study for rotorcraft avionics bay cooling

7. USE OF ARTIFICIAL NEURAL NETWORK IN ROTORCRAFT COOLING SYSTEM

8. EFFECTS OF PIN FIN SHAPE AND SIZE ON TURBINE BLADE TRAILING EDGE FLOW AND HEAT TRANSFER

9. Uncertainty Analysis of Heat Transfer Predictions Using Statistically Modeled Data From a Cooled 1-1/2 Stage High-Pressure Transonic Turbine

10. Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine-Part II: Effect of Cooling Variation on the Vane Airfoil and Inner End Wall

11. Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine-Part I: Experimental Configuration and Data Review With Inlet Temperature Profile Effects

12. Validation of MISES Two-Dimensional Boundary Layer Code for High-Pressure Turbine Aerodynamic Design

1. Data-Driven Optimization of Transition Modeling for Improved Boundary Layer Predictions

2. Computational Investigation of Perpendicular Blade-Vortex Interaction

3. Estimating Sweet Spot for UAV Formation Flight Using Vortex Lattice Method and Machine Learning

4. Numerical Simulation of Spray Characteristics of Doublet Injectors

5. Investigation of a rotor blade with tip cooling subject to a nonuniform temperature profile

6. Gas Turbine Blade Cooling Technology, Advances, and Challenges

7. EFFECT OF TURBINE BLADE TIP COOLING CONFIGURATION ON TIP LEAKAGE FLOW AND HEAT TRANSFER

8. Comparison of Temperature Profile and Heat Transfer Predictions With Statistically Modeled Data From a Cooled 1 1 2 Stage High Pressure Transonic Turbine

9. Heat Transfer for the Film Cooled Vane of a 1 1 2 Stage High Pressure Transonic Turbine Part I Experimental Configuration and Data Review With Inlet Temperature Profile Effects

10. Heat Transfer for the Film Cooled Vane of a 1 1 2 Stage High Pressure Transonic Turbine Part II Effect of Cooling Variation on the Vane Airfoil and Inner Endwall

11. Validation of MISES 2 D Boundary Layer Code for High Pressure Turbine Aerodynamic Design

12. Flow Around Helicopter Blade Tip Sections Using a 2D Particle Image Velocimeter Part I

13. Flow Around Helicopter Blade Tip Sections Using a 3D Stereoscopic Particle Image Velocimeter Part II

Yayın

Yayın (WoS)

Yayın (Scopus)

Atıf (WoS)

H-İndeks (WoS)

Atıf (Scopus)

H-İndeks (Scopus)

Atıf (Scholar)

H-İndeks (Scholar)

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