ACTIVE CONTROL OF FLOW PAST OVER NACA 0021 THROUGH LEADING EDGE MOMENTUM INJECTION USING ROTATING CYLINDER: A COMPARATIVE INVESTINGATION BETWEEN NUMERICAL & EXPERIMENTAL ANALYSIS/
محفوظ في:
| المؤلف الرئيسي: | |
|---|---|
| مؤلف مشترك: | |
| مؤلفون آخرون: | , |
| التنسيق: | كتاب |
| اللغة: | الإنجليزية |
| منشور في: |
Dhaka:
MIST AE DEPT
c 2018
|
| الموضوعات: | |
| الوسوم: |
لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!
|
مواد مشابهة: ACTIVE CONTROL OF FLOW PAST OVER NACA 0021 THROUGH LEADING EDGE MOMENTUM INJECTION USING ROTATING CYLINDER: A COMPARATIVE INVESTINGATION BETWEEN NUMERICAL & EXPERIMENTAL ANALYSIS/
- STUDY OF THE INFLUENCE OF LEADING EDGE ROTATING CYLINDER ON THE PERFORMANCE OF A SYMMETRIC AEROFOIL
- CHARACTERISTIC ANALYSIS OF NACA 0018 AND NACA 2412 AIRFOIL WITH LEADING EDGE AND TRAILING EDGE ROTATING CYLINDER /
- STUDY OF MOMENTUM INJENCTION: EFFECT OF CLEARENCE BETWEEN ROTATING CYLINDER AND GROOVED AIRFOIL /
- DETERMINATION OF SOAKED AND UNSOAKED CBR VALUES FOR DIFFERENT SOIL TYPE/
- DESIGN AND OPTIMIZATION OF LOW SPEED WIND TURBINE WITH MOMENTUM INJECTION /
- DETERMINATION OF FLOW CHARACTERISTICS AND PERFORMANCE ANALYSIS OF THE NON-ROTATING & ROTATING CYLINDER /