CHARACTERISTIC ANALYSIS OF NACA 0018 AND NACA 2412 AIRFOIL WITH LEADING EDGE AND TRAILING EDGE ROTATING CYLINDER /
محفوظ في:
| مؤلف مشترك: | |
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| مؤلفون آخرون: | , |
| التنسيق: | كتاب |
| اللغة: | الإنجليزية |
| منشور في: |
Dhaka :
AE DEPT. MIST,
c2021.
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| الموضوعات: | |
| الوسوم: |
لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!
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مواد مشابهة: CHARACTERISTIC ANALYSIS OF NACA 0018 AND NACA 2412 AIRFOIL WITH LEADING EDGE AND TRAILING EDGE ROTATING CYLINDER /
- A NUMERICAL ANALYSIS ON THE AERODYNAMIC CHARACTERISTICS OF NACA 0015 AND NACA 2412 AEROFOILS WITH CURVED TRAILING-EDEG PLANFORM /
- ACTIVE CONTROL OF FLOW PAST OVER NACA 0021 THROUGH LEADING EDGE MOMENTUM INJECTION USING ROTATING CYLINDER: A COMPARATIVE INVESTINGATION BETWEEN NUMERICAL & EXPERIMENTAL ANALYSIS/
- AERODYNAMICS PERFORMANCE ANALYSIS OF 2D AIRFOIL/ NACA 4418 INCORPORATING WITH ROTATING CYLINDER /
- STUDY OF THE INFLUENCE OF LEADING EDGE ROTATING CYLINDER ON THE PERFORMANCE OF A SYMMETRIC AEROFOIL
- A STUDY OF STATIC EXTENDED TRAILING EDGE FOR LIFT ENHANCEMENT /
- COMPARATIVE STUDY OF BLOWING AND SUCTION SLOT GEOMETRY OPTIMIZATION ON NACA 0015 AND NACA 2412 AIRFOIL /