STUDY OF THE FLOW FIELD ON THE UPPER SURFACE OF NACA 0015 & NACA 2418 AT DIFFERENT AANGLE OF ATTACK /
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| Συγγραφή απο Οργανισμό/Αρχή: | |
| Άλλοι συγγραφείς: | , |
| Μορφή: | Βιβλίο |
| Γλώσσα: | Αγγλικά |
| Έκδοση: |
Dhaka :
AE DEPT. MIST,
c2018.
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Παρόμοια τεκμήρια: STUDY OF THE FLOW FIELD ON THE UPPER SURFACE OF NACA 0015 & NACA 2418 AT DIFFERENT AANGLE OF ATTACK /
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- EXPERIMENTAL STUDY OF FLOW VELOCITY AND DIRECTION AROUND NACA 0012 & NACA 0015 AIRFOILEXPERIMENTAL STUDY OF FLOW VELOCITY AND DIRECTION AROUND NACA 0012 & NACA 0015 AIRFOIL
- COMPARATIVE STUDY OF BLOWING AND SUCTION SLOT GEOMETRY OPTIMIZATION ON NACA 0015 AND NACA 2412 AIRFOIL /
- EXPERIMENTAL STUDY OF FLOW VELOCITY AND DIRECTION AROUND NACA 0012 & NACA 0015 AIRFOIL
- A COMPARATIVE STUDY OF AERODYNAMIC CHARACTERISTICS OF NACA 0015 AND NACA 4415 AIRFOILS AT VARIOUS REYNOLDS NUMBER /
- A NUMERICAL ANALYSIS ON THE AERODYNAMIC CHARACTERISTICS OF NACA 0015 AND NACA 2412 AEROFOILS WITH CURVED TRAILING-EDEG PLANFORM /