An experimental and numerical investigation on boundary layer control with blown flaps incorporating Coanda effect
محفوظ في:
| المؤلفون الرئيسيون: | , |
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| التنسيق: | كتاب |
| اللغة: | الإنجليزية |
| منشور في: |
Dhaka, Bangladesh :
Department of Mechanical Engineering, Military Institute of Science and Technology,
@ February 2023.
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| الطبعة: | Bachelor's thesis |
| الوسوم: |
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مواد مشابهة: An experimental and numerical investigation on boundary layer control with blown flaps incorporating Coanda effect
- Boundary layer theory
- EFFECT OF MOMENTUM INJECTION ON THE PERFORMANCE OF AIRFOIL (MOVING SURFACE BOUNDARY LAYER CONTROL /
- AN EXPERIMENTAL AND NUMERICAL INVESTIGATION ON EFFECT OF SHAPES AND ARRANGEMENT OF SOLID BODIES IN WIND LOADING
- AN EXPERIMENTAL AND NUMERICAL INVESTIGATION ON EFFECT OF SHAPES AND ARRANGEMENT OF SOLID BODIES IN WIND LOADING /
- STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY-LAYER CONTROL (MSBC) ON A DOUBLE CYLINDER CONFIGURATION : NACA 0018 AIRFOIL /
- STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY LAYER CONTROL ( MSBC) ON SINGLE & DOUBLE CYLINDER CONFIGURATION NACA 23018 AIRFOIL /