CHARACTERISTIC ANALYSIS OF NACA 0018 AND NACA 2412 AIRFOIL WITH LEADING EDGE AND TRAILING EDGE ROTATING CYLINDER /

समान संसाधन

• A NUMERICAL ANALYSIS ON THE AERODYNAMIC CHARACTERISTICS OF NACA 0015 AND NACA 2412 AEROFOILS WITH CURVED TRAILING-EDEG PLANFORM /
  द्वारा: Nuzhat, Anika
  प्रकाशित: (2022)
• ACTIVE CONTROL OF FLOW PAST OVER NACA 0021 THROUGH LEADING EDGE MOMENTUM INJECTION USING ROTATING CYLINDER: A COMPARATIVE INVESTINGATION BETWEEN NUMERICAL & EXPERIMENTAL ANALYSIS/
  द्वारा: Romeo, Shafi-Al-Salman
  प्रकाशित: (2018)
• AERODYNAMICS PERFORMANCE ANALYSIS OF 2D AIRFOIL/ NACA 4418 INCORPORATING WITH ROTATING CYLINDER /
  द्वारा: Prince, Md Raqibul Hasan
  प्रकाशित: (2018)
• STUDY OF THE INFLUENCE OF LEADING EDGE ROTATING CYLINDER ON THE PERFORMANCE OF A SYMMETRIC AEROFOIL
  द्वारा: FAISAL, KH. MD.
  प्रकाशित: (2017)
• A STUDY OF STATIC EXTENDED TRAILING EDGE FOR LIFT ENHANCEMENT /
  द्वारा: Rahman, Md. Azizur
  प्रकाशित: (2022)