ACTIVE CONTROL OF FLOW PAST OVER NACA 0021 THROUGH LEADING EDGE MOMENTUM INJECTION USING ROTATING CYLINDER: A COMPARATIVE INVESTINGATION BETWEEN NUMERICAL & EXPERIMENTAL ANALYSIS/
Gardado en:
| Autor Principal: | |
|---|---|
| Autor Corporativo: | |
| Outros autores: | , |
| Formato: | Libro |
| Idioma: | inglés |
| Publicado: |
Dhaka:
MIST AE DEPT
c 2018
|
| Subjects: | |
| Tags: |
Sen Etiquetas, Sexa o primeiro en etiquetar este rexistro!
|
Títulos similares: 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 /