Metrikler
Yayın
25
Açık Erişim
4
Biyografi
Harika S. Kahveci
is an Associate Professor at the Aerospace Engineering Department at METU,
Turkey. She received her Ph.D in Mechanical Engineering from The Ohio State
University in 2010, her M.S. degree in Aerospace Engineering from Penn State
University in 2004, and her B.S. degree in 2002 from the same department of
METU where she is currently teaching. She worked at General Electric Company
for 11 years undertaking various responsibilities and worked on the design of
aerodynamics, heat transfer and blade cooling of gas turbines. She is the
recipient of the UTSR Gas Turbine Industrial Fellowship Award (2003), the
Critical Difference for Women Fellowship (2008), and the ASME Best Technical
Paper Award (2013), and received several company awards at GE. She was awarded the
ASME Gas Turbine Award in 2015. Her research
interests include design
of gas turbines, engine
aerothermodynamics and cooling systems, computational fluid dynamics and
experimental techniques.
Araştırma Alanları
Makina Mühendisliği
Mühendislik ve Teknoloji
Makaleler
Tümü (12)
SCI-E, SSCI, AHCI (11)
SCI-E, SSCI, AHCI, ESCI (11)
Scopus (11)
TRDizin (2)
2024
20241. 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)
2021
20212. 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)
2020
20203. 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)
2019
20194. 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)
2019
20195. 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)
2019
20196. 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)
2019
20197. 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)
2019
20198. 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)
2014
20149. 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)
2013
201310. 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)
2013
201311. 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)
2009
200912. 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
2025
20251. 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)
2025
20252. 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)
2023
20233. 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)
2021
20214. 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)
2020
20205. 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)
2019
20196. 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)
2019
20197. 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)
2013
20138. 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)
2011
20119. 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)
2011
201110. 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)
2007
200711. Validation of MISES 2 D Boundary Layer Code for High Pressure Turbine Aerodynamic Design
Andrew P., Kahveci H. S.
Volume 6: ASME Turbo Expo 2007, Parts A and B, Montreal, Kanada, 14 - 19 Mayıs 2007, cilt.6, ss.879-893, (Tam Metin Bildiri)
2006
200612. Flow Around Helicopter Blade Tip Sections Using a 2D Particle Image Velocimeter Part I
Kahveci H. S., Camcı C.
The Eleventh International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-11), Honolulu, Hawaii, Hawaii, Amerika Birleşik Devletleri, 26 Şubat - 02 Mart 2006, cilt.2, ss.718-726, (Tam Metin Bildiri)
2006
200613. Flow Around Helicopter Blade Tip Sections Using a 3D Stereoscopic Particle Image Velocimeter Part II
Kahveci H. S., Camcı C.
The Eleventh International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-11), Honolulu, Hawaii, Hawaii, Amerika Birleşik Devletleri, 26 Şubat - 02 Mart 2006, cilt.2, ss.727-735, (Tam Metin Bildiri)
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