EFFECT OF ROTATING CYLINDER ON THE PERFORMANCE OF SYMMETRIC AIRFOIL: “AN EXPERIMENTAL STUDY /

Enregistré dans:

Détails bibliographiques
Auteur principal:	Huda, Md. Nurul
Collectivité auteur:	Supervised by Group Captain Md. Abdur Salam (Professor, Department of Aeronautical Engineering, MIST, Dhaka.)
Autres auteurs:	Tabassum Ahamed, S M Shakil Ahamed
Format:	Livre
Langue:	anglais
Publié:	Dhaka : AE DEPT MIST , c 2015.
Sujets:	Thesis Paper of AE in B.Sc Prog. Aeronautical Engineering.
Tags:	Ajouter un tag Pas de tags, Soyez le premier à ajouter un tag!

Documents similaires: EFFECT OF ROTATING CYLINDER ON THE PERFORMANCE OF SYMMETRIC AIRFOIL: “AN EXPERIMENTAL STUDY /

Aperçu
AERODYNAMICS PERFORMANCE ANALYSIS OF 2D AIRFOIL/ NACA 4418 INCORPORATING WITH ROTATING CYLINDER /
Aperçu
STUDY OF MOMENTUM INJENCTION: EFFECT OF CLEARENCE BETWEEN ROTATING CYLINDER AND GROOVED AIRFOIL /
Aperçu
EXPERIMENTAL STUDY OF FLOW AROUND A ROTATING CYLINDER /
Aperçu
EXPERIMENTAL STUDY OF FLOW AROUND A ROTATING CYLINDER /
Aperçu
DETERMINATION OF FLOW CHARACTERISTICS AND PERFORMANCE ANALYSIS OF THE NON-ROTATING & ROTATING CYLINDER /
Aperçu
DEVELOPMENT OF AN EXPERIMENTAL SETUP FOR ANALYZING THE INFLUENCE OF MAGNUS EFFECT ON THE PERFORMANCE OF AIRFOIL /
Aperçu
EXPERIMENTAL STUDY OF CO-ROTATING SWIRLING JETS /
Aperçu
STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY LAYER CONTROL ( MSBC) ON SINGLE & DOUBLE CYLINDER CONFIGURATION NACA 23018 AIRFOIL /
Aperçu
EXPERIMENTAL STUDY OF FLOW CHARACTERISTICS OF ROUGHENED SURFACE AIRFOILS /
Aperçu
STUDY OF THE INFLUENCE OF LEADING EDGE ROTATING CYLINDER ON THE PERFORMANCE OF A SYMMETRIC AEROFOIL
Aperçu
A COMPARISON OF EXPERIMENTAL WITH SIMULATION EFFECTIVE OF NACA 0012 AIRFOIL WITH BARE /
Aperçu
CHARACTERISTIC ANALYSIS OF NACA 0018 AND NACA 2412 AIRFOIL WITH LEADING EDGE AND TRAILING EDGE ROTATING CYLINDER /
Aperçu
EXPERIMENTAL STUDY OF FLOW CHARACTERISTICS AROUND NACA 4418 AND NACA 0012 AIRFOIL /
Aperçu
EFFECT OF MOMENTUM INJECTION ON THE PERFORMANCE OF AIRFOIL (MOVING SURFACE BOUNDARY LAYER CONTROL /
Aperçu
THE EXPERIMENTAL STUDY OF THE AERODYNAMIC CHARACTERISTICS OF THE AIRFOIL OF FOUGA MAGISTER 170 /
Aperçu
ACTIVE CONTROL OF FLOW PAST OVER NACA 0021 THROUGH LEADING EDGE MOMENTUM INJECTION USING ROTATING CYLINDER: A COMPARATIVE INVESTINGATION BETWEEN NUMERICAL & EXPERIMENTAL ANALYSIS/
Aperçu
COMPARATIVE ASSESSMENT OF TURBULENCE OF IMPROVED PERFORMANCE OF NAC 0012 AIRFOIL WITH MSBLC /
Aperçu
EXPERIMENTAL STUDY OF FLOW AROUND A ROTATING CYLINDER
Aperçu
EXPERIMENTAL STUDY OF FLOW VELOCITY AND DIRECTION AROUND NACA 0012 & NACA 0015 AIRFOIL /
Aperçu
EFFECT OF CROSS –SECTIONAL SHAPES ON FREE JET CHARACTERIZATION NUMERICAL AND EXPERIMENTAL INVESTIGATION FEASIBLE AND PERFORMANCE OF DIFFERENT EXHAUST GEOMETRY /
Aperçu
STUDY OF FLOW BEHIND A CIRCULAR CYLINDER AND AN AIROFOIL /
Aperçu
COMPARATIVE AND ASSESSMENT OF VARIOUS TURBULENCE MODELS AND IMPROVED PERFORMANCE OF NACA 0010 AIRFOIL WITH MSBLC /
Aperçu
INVESTIGATION OF THE EFFECT OF DIFFERENT AIRFOIL SHAPED FUSELAGE ON THE PERFORMANCE OF AN UNMANNED AIR VEHICLE /
Aperçu
EXPERIMENTAL STUDY OF AERODYNAMIC CO-EFFICIENTS, CO-EFFICIENT OF PRESSURE AND-FIELD AROUND 0012 AIRFOIL /