Ali Dinc

Geothermal Heat Pump for Space Cooling and Heating in Kuwaiti Climate. Y Gharbia, JF Derakhshandeh, AM Amer, A Dinc Processes 12 (5), 910, 2024.

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Preliminary Design Study of a Micro Blended-Wing-Body Airplane: a Student Project. A Dinc, N Alsanea, H Alshammari, M Mohsen, A Maayouf, M Alhumaidi, ... International Review of Aerospace Engineering 17 (1), 19-28, 2024.

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Reliability of different nanofluids and different micro-channel configurations on the heat transfer augmentation. I Elbadawy, A Alhajri, M Doust, Y Almulla, M Fayed, A Dinc, M Abouelela, ... Processes 11 (3), 652, 2023.

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Multiple Linear Regression Analysis-Based Weight Estimation of Turbofan Engines. A Dinc, NP Alakoc, Y Gharbia, M Abouelela, N Alsanea, AM Amer, K Nag International Review of Aerospace Engineering 16 (1), 22-28, 2023.

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Effect of Al2O3, SiO2, and ZnO Nanoparticle Concentrations Mixed with EG-Water on the Heat Transfer Characteristics through a Microchannel. I Elbadawy, F Alali, JF Derakhshandeh, A Dinc, M Abouelela, W Al-Kouz Processes 11 (7), 2015, 2023.

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Effect of Refrigerated Inlet Cooling on Greenhouse Gas Emissions for a 250 MW Class Gas Turbine Engine. A Dinc, A Mamedov, ET Duran, F Abbassi, I Elbadawy, K Nag, ... Aerospace 10 (10), 833, 2023.

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Structural Design and Stress Analysis of a Micro Aircraft Wing in a Student Competition. A Dinc, A Almukhaizeem, H Ahmad, Y Alotaibi, A Almutairi, M Abouelela, ... International Review of Aerospace Engineering 16 (6), 223-232, 2023.

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Tensile Test Optimization Using the Design of Experiment and Soft Computing. M Moayyedian, MRC Qazani, V Cvorovic, F Asi, A Mussin, ... Processes 11 (11), 3106, 2023.

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Investigation of Turbofan Engine Emissions at Different Cruise Conditions for Greener Flights. A Dinc, I Elbadawy, M Fayed, K Nag, R Taher, Y Gharbia International Symposium On Sustainable Aviation, 321-327, 2023.

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Dynamic Modeling of Main Landing Gear of a High-Altitude Long Endurance UAV. A Dinc, Y Gharbia New Achievements in Unmanned Systems, 239-248, 2023.

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A performance-based parametric design exploration tool for student aircraft design projects. A Dinc, MB Fahad, A Boshehri, A Abdulghfar, A Hamadah, F Alenezi, ... International Review of Aerospace Engineering 16 (2), 73-82, 2023.

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Turbofan Engine Weight Estimation Using Regression Analysis. A Dinc, NP Alakoc, Y Gharbia, M Abouelela, N Alsanea, AM Amer 2nd International World Energy Conference, 208-209, 2022.

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Exergy analysis of a turboprop engine at different flight altitude and speeds using novel consideration. A Dinc, Y Gharbia International Journal of Turbo & Jet-Engines 39 (4), 599-604, 2022.

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Thermodynamic-based environmental and enviroeconomic assessments of a turboprop engine used for freight aircrafts under different flight phases. A Dinc, H Caliskan, S Ekici, Y Sohret Journal of Thermal Analysis and Calorimetry 147 (22), 12693-12707, 2022.

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Optimization of surface quality and machining time in micro-milling of glass. A Dinc, A Mamedov Aircraft Engineering and Aerospace Technology 95 (5), 676-686, 2022.

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Exergy mapping of a UAV through a reconnaissance flight envelope. Y S o hret, A Dinc Journal of Aeronautics and Space Technologies 15 (1), 35-45, 2022.

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Performance Modelling of Landing Gear and Suspension System of a Flying Car for Landing and Bump Passing Manoeuvres. M O tku r, D Ali Engineer and Machinery 63 (709), 616-632, 2022.

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Design and Optimization of Control Arm in a Solar Car Using QFD. M Moayyedian, A Dinc, A Alsarraf, W Hamouda, A Almutairi, A Bushehri, ... New Approaches in Engineering Research Vol. 14, 59-66, 2021.

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Optimization of Injection-Molding Process for Thin-Walled Polypropylene Part Using Artificial Neural Network and Taguchi Techniques. M Moayyedian, A Dinc, A Mamedov Polymers 13 (23), 4158, 2021.

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Investigating the green performance limits of a cargo aircraft engine during flight: a thermo-environmental evaluation. Y S o hret, S Ekici, A Dinc Energy Sources, Part A: Recovery, Utilization, and Environmental Effects, 1-16, 2021.

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Emissions prediction of an aero-piston gasoline engine during surveillance flight of an unmanned aerial vehicle. A Dinc, M Otkur Aircraft Engineering and Aerospace Technology 93 (3), 462-472, 2021.

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Performance Improvement of a 43 MW Class Gas Turbine Engine with Inlet Air Cooling. A Dinc, I Elbadawy, M Fayed, R Taher, JF Derakhshandeh, Y Gharbia International Journal of Emerging Trends in Engineering Research 9 (5), 2021.

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The effect of flight and design parameters of a turbofan engine on global warming potential. A Dinc IOP Conference Series: Materials Science and Engineering 1051 (1), 012051, 2021.

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Performance Degradation of a 43 MW Class Gas Turbine Engine in Kuwait Climate. A Dinc, R Taher, JF Derakhshandeh, M Fayed, I Elbadawy, Y Gharbia International Research Journal of Innovations in Engineering and Technology ..., 2021.

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A sizing tool for the preliminary design of an unmanned aerial vehicle for student projects. A Dinc, Y Gharbia, A Bushehri, F Al-Sarraf, A Al-Ali, AMA Alsaidi, ... International Journal of Research Publications 77 (1), 68-72, 2021.

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Metering pin diameter optimization of an aircraft landing gear shock absorber. A Dinc Eskis ehir Teknik U niversitesi Bilim ve Teknoloji Dergisi B-Teorik Bilimler 9 ..., 2021.

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NOx emissions of turbofan powered unmanned aerial vehicle for complete flight cycle. D Ali Chinese Journal of Aeronautics 33 (6), 1683-1691, 2020.

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Global warming potential optimization of a turbofan powered unmanned aerial vehicle during surveillance mission. A Dinc, I Elbadawy Transportation Research Part D: Transport and Environment 85, 102472, 2020.

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Exergy analysis of a three-spool turboprop engine during the flight of a cargo aircraft. A Dinc, Y S o hret, S Ekici Aircraft Engineering and Aerospace Technology 92 (10), 1495-1503, 2020.

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Optimization of electric vehicle battery size and reduction ratio using genetic algorithm. A Dinc, M Otkur 2020 11th International Conference on Mechanical and Aerospace Engineering ..., 2020.

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Sizing of a Turboprop Engine Powered High Altitude Unmanned Aerial Vehicle and Its Propulsion System for an Assumed Mission Profile in Turkey. D Ali International Journal of Aviation Science and Technology 1 (01), 5-8, 2020.

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Global warming potential estimations of a gas turbine engine and effect of selected design parameters. A Dinc, Y Gharbia ASME International Mechanical Engineering Congress and Exposition 84560 ..., 2020.

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A Performance Review of a High Altitude Long Endurance Drone. A Dinc, R Taher, M Moayyedian, A Bushehri, A Alruwayeh, A Alsaeedi, ... International Journal of Progressive Sciences and Technologies 24 (1), 32-39, 2020.

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Preliminary design of a radio-controlled micro aircraft for student competition. A Dinc, Y Gharbia, M AlShammari, A AlRasheedi, S AlQallaf, M AlIbrahim, ... Global Journal of Engineering and Technology Advances 4 (3), 064-069, 2020.

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Effects of Spring and Damper Elements in Aircraft Landing Gear Dynamics. A Dinc, Y Gharbia International Journal of Recent Technology and Engineering 8 (5), 4265-4269, 2020.

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Predicting Maximum Endurance of a High Altitude Long Endurance UAV with Taguchi Method. A Dinc, M Moayyedian International Journal of Innovations in Engineering Research and Technology ..., 2020.

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Preliminary Sizing and Performance Calculations of Unmanned Air Vehicles. A Dinc Automated Systems in the Aviation and Aerospace Industries, 242-272, 2019.

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Improving Flight Endurance of a UAV by Employing Porous Wing Tip. A Dinc, Y Gharbia American Journal of Engineering Research 7 (11), 177-181, 2018.

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ECOLOGICAL ASSESSMENT OF A TURBOFAN ENGINE OF AN UAV AT SURVEILLANCE ALTITUDE. Y S o hret, A Dinc , TH Karakoc International Symposium on Sustainable Aviation 10 (13), 2017.

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Optimization of turboprop ESFC and NOx emissions for UAV sizing. A Dinc Aircraft Engineering and Aerospace Technology 89 (3), 375-383, 2017.

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Optimization of a turboprop UAV for maximum loiter and specific power using genetic algorithm. A Dinc International Journal of Turbo & Jet-Engines 33 (3), 265-273, 2016.

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Military Turbofan Engine Development Project Cost Estimation and Technology Readiness Level Based Risk Factors in a Sustainable Acquisition Management System Example. D Ali Su rdu ru lebilir Havac l k Aras t rmalar Dergisi 1 (1), 11-18, 2016.

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Calculation of burner efficiency with the help of exhaust emissions for an 80 kN class turbofan engine. TH KARAKOC , Y S O HRET, ALI DI NC III. National Aviation Technologies and Applications Congress, 2015.

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An Application of a Computerized Data Acquisition System in Testing of an Auxiliary Power Unit. A Dinc International Journal of Scientific & Engineering Research 6 (5), 1057-1064, 2015.

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Exergy analysis of a turbofan engine for an unmanned aerial vehicle during a surveillance mission. Y S o hret, A Dinc , TH Karakoc Energy 93, 716-729, 2015.

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Sizing of a Turboprop Unmanned Air Vehicle and its Propulsion System. A Dinc Journal of Thermal Science & Technology 35 (2), 2015.

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Design and Implementation of a Data Acquisition System for Testing of Gas Turbine Engines. A Dinc Journal of Multidisciplinary Engineering Science and Technology 2 (3), 2015.

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An engine mounting system. A Dinc, ET Topal TR Patent TR 2014 13013 B, 2014.

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Investigation of effect of exhaust nozzle exit area on engine performance. O Ates , T Yasa, E Eken, F Karago z, O Dog ruer, A Dinc 7th National Aeronautics and Space Conference, 2013.

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Optimization with elitist genetic algorithm method in preliminary design of unmanned air vehicle & its propulsion system. A Dinc, H Bug dayci, O Uzol International Unmanned Vehicles Workshop UVW2010, 2010.

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Sizing of a high altitude long endurance (HALE) UAV & its propulsion system for a given Turkish mission profile. A Dinc, H Bug dayci, O Uzol 5th National Aeronautics and Space Conference, 2009.

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