İçeriğe geç
akaturk Akademik ölçüm

Akademisyen

MUSTAFA PERÇİN

DOÇENT

ORTA DOĞU TEKNİK ÜNİVERSİTESİ MÜHENDİSLİK FAKÜLTESİ HAVACILIK VE UZAY MÜHENDİSLİĞİ BÖLÜMÜ

  • Ana Dal Mühendislik Temel Alanı
  • Yan Dal Uçak-Havacılık-Uzay Mühendisliği

Kayıtlı çıktılara kısa bakış — ayrıntılar aşağıda.

  • Makale 27
  • Proje 0
  • Kitap 0
  • Bildiri 0
  • Patent 0
  • Sanatsal 0
Scopus (SJR) Q1 19 Q2 4 Q3 2 Q4 0
WoS (JCR) Q1 9 Q2 12 Q3 2 Q4 2
TR Index 2 makale

Makaleler

YÖKSİS ve OpenAlex kaynak ayrımıyla makaleler; quartile ve TR Index ile daraltabilirsiniz.

Dizin filtreleri

Toplam 27 yayın

Makale listesi

  1. 2025 An experimental investigation of the effects of a boundary layer inflow on the wake characteristics of a model wind turbine and a porous disk Journal of Renewable and Sustainable Energy DOI 10.1063/5.0249345 YÖKSİS SJR Q3 JCR Q4
  2. 2023 An integrated pipeline for building performance analysis: Daylighting, energy, natural ventilation, and airborne contaminant dispersion Journal of Building Engineering DOI 10.1016/j.jobe.2023.106991 YÖKSİS SJR Q1 JCR Q1
  3. 2023 On the wake characteristics of a model wind turbine and a porous disc: Effects of freestream turbulence intensity Renewable Energy DOI 10.1016/j.renene.2023.05.002 YÖKSİS SJR Q1 JCR Q1
  4. 2023 Tip Vortex Meandering Characteristics of a Model Helicopter Rotor with Different Tip Shapes American Institute of Aeronautics and Astronautics (AIAA) DOI 10.2514/1.J062552 YÖKSİS SJR Q1 JCR Q2
  5. 2023 Leading-Edge Vortex Characteristics of Surging-Translating Flexible Wings Havacılık ve Uzay Teknolojileri Dergisi DOI https://jast.hho.msu.edu.tr/index.php/JAST/article/view/528/373 YÖKSİS TR Index
  6. 2021 Asymmetric vortex shedding in the wake of an abruptly expanding annular jet EXPERIMENTS IN FLUIDS DOI 10.1007/s00348-021-03177-9 YÖKSİS SJR Q1 JCR Q2
  7. 2021 Effects of inflow boundary layer on the wake of a radially non-uniform porous disk JOURNAL OF RENEWABLE AND SUSTAINABLE ENERGY DOI 10.1063/5.0045404 YÖKSİS SJR Q3 JCR Q4
  8. 2021 Experimental investigation of tip anhedral effects on the aerodynamics of a model helicopter rotor in hover AEROSPACE SCIENCE AND TECHNOLOGY DOI 10.1016/j.ast.2021.106671 YÖKSİS SJR Q1 JCR Q1
  9. 2020 Single- and double-helix vortex breakdown as two dominant global modes in turbulent swirling jet flow JOURNAL OF FLUID MECHANICS DOI 10.1017/jfm.2019.872 YÖKSİS SJR Q1 JCR Q1
  10. 2020 Numerical Investigation of Propeller-Frame Arm Interaction in Hovering Flight Havacılık ve Uzay Teknolojileri Dergisi DOI https://jast.hho.msu.edu.tr/index.php/JAST/article/view/422/319 YÖKSİS TR Index
  11. 2019 Accurate position control of a flapping-wing robot enabling free-flight flow visualisation in a wind tunnel International Journal of Micro Air Vehicles DOI http://journals.sagepub.com/doi/10.1177/1756829319833683 YÖKSİS SJR Q2 JCR Q3
  12. 2018 Three-dimensional flow and load characteristics of flexible revolving wings Experiments in Fluids DOI 10.1007/s00348-018-2613-1 YÖKSİS SJR Q1 JCR Q2
  13. 2018 Numerical Simulation of a Flapping Micro Aerial Vehicle Through Wing Deformation Capture AIAA Journal DOI 10.2514/1.J056482 YÖKSİS SJR Q1 JCR Q2
  14. 2018 Double helix vortex breakdown in a turbulent swirling annular jet flow PHYSICAL REVIEW FLUIDS DOI 10.1103/PhysRevFluids.3.034703 YÖKSİS SJR Q1 JCR Q2
  15. 2018 Flow Visualization around a Flapping-Wing Micro Air Vehicle in Free Flight Using Large-Scale PIV Aerospace DOI 10.3390/aerospace5040099 YÖKSİS SJR Q2 JCR Q2
  16. 2017 Flow Structures Around a Flapping-Wing Micro Air Vehicle Performing a Clap-and-Peel Motion AIAA Journal DOI 10.2514/1.J055146 YÖKSİS SJR Q1 JCR Q2
  17. 2017 Analysis of the pressure fields in a swirling annular jet flow Experiments in Fluids DOI 10.1007/s00348-017-2446-3 YÖKSİS SJR Q1 JCR Q2
  18. 2017 Numerical Simulation of a Flexible X-Wing Flapping-Wing Micro Air Vehicle AIAA Journal DOI 10.2514/1.J054816 YÖKSİS SJR Q1 JCR Q2
  19. 2016 Deconvolution Kalman filtering for force measurements of revolving wings Measurement Science and Technology DOI 10.1088/0957-0233/27/9/095302 YÖKSİS SJR Q1 JCR Q2
  20. 2016 Experimental Investigation of Aerodynamics of Flapping-Wing Micro-Air-Vehicle by Force and Flow-Field Measurements AIAA Journal DOI 10.2514/1.J054403 YÖKSİS SJR Q1 JCR Q1

Akademisyenlere dön