EXPERIMENTAL STUDY OF FLOW AROUND A ROTATING CYLINDER

Experimental Study of Flow Around a Rotating Cylinder

में बचाया:

ग्रंथसूची विवरण
मुख्य लेखकों:	MOON, MITHILA ISLAM, SHABNAM, HASSAN MAYESHA, MOHSINA AKHTER, SYEDA
स्वरूप:	थीसिस
भाषा:	अंग्रेज़ी
प्रकाशित:	2025
ऑनलाइन पहुंच:	http://dspace.mist.ac.bd:8080/xmlui/handle/123456789/932
टैग:	टैग जोड़ें कोई टैग नहीं, इस रिकॉर्ड को टैग करने वाले पहले व्यक्ति बनें!

समान संसाधन: EXPERIMENTAL STUDY OF FLOW AROUND A ROTATING CYLINDER

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EXPERIMENTAL STUDY OF FLOW AROUND A ROTATING CYLINDER /
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EXPERIMENTAL STUDY OF FLOW AROUND A ROTATING CYLINDER /
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DETERMINATION OF FLOW CHARACTERISTICS AND PERFORMANCE ANALYSIS OF THE NON-ROTATING & ROTATING CYLINDER /
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EFFECT OF ROTATING CYLINDER ON THE PERFORMANCE OF SYMMETRIC AIRFOIL: “AN EXPERIMENTAL STUDY /
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EXPERIMENTAL STUDY OF CO-ROTATING SWIRLING JETS /
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STUDY OF THE INFLUENCE OF LEADING EDGE ROTATING CYLINDER ON THE PERFORMANCE OF A SYMMETRIC AEROFOIL
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STUDY OF FLOW BEHIND A CIRCULAR CYLINDER AND AN AIROFOIL /
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EXPERIMENTAL STUDY OF FLOW CHARACTERISTICS AROUND NACA 4418 AND NACA 0012 AIRFOIL /
त्वरित देखें
STUDY OF MOMENTUM INJENCTION: EFFECT OF CLEARENCE BETWEEN ROTATING CYLINDER AND GROOVED AIRFOIL /
त्वरित देखें
EXPERIMENTAL STUDY OF FLOW VELOCITY AND DIRECTION AROUND NACA 0012 & NACA 0015 AIRFOIL
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EXPERIMENTAL STUDY OF FLOW VELOCITY AND DIRECTION AROUND NACA 0012 & NACA 0015 AIRFOIL /
त्वरित देखें
EXPERIMENTAL STUDY OF FLOW CHARACTERISTICS AROUND DIFFERENT SHAPED BODIES AND TO FIND THE RESULTING DRAG /
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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
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UNDERSTANDING THE BEHAVIOUR OF LAUNCHING APRONS AROUND ABUTMENT: AN EXPERIMENTAL STUDY
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ACTIVE CONTROL OF FLOW PAST OVER NACA 0021 THROUGH LEADING EDGE MOMENTUM INJECTION USING ROTATING CYLINDER: A COMPARATIVE INVESTINGATION BETWEEN NUMERICAL & EXPERIMENTAL ANALYSIS/
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NUMERICAL SIMULATION OF FLOW AROUND UNDERWATER BODIES /
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AERODYNAMICS PERFORMANCE ANALYSIS OF 2D AIRFOIL/ NACA 4418 INCORPORATING WITH ROTATING CYLINDER /
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EXPERIMENTAL STUDY OF AERODYNAMIC CO-EFFICIENTS, CO-EFFICIENT OF PRESSURE AND-FIELD AROUND 0012 AIRFOIL /
त्वरित देखें
CHARACTERISTIC ANALYSIS OF NACA 0018 AND NACA 2412 AIRFOIL WITH LEADING EDGE AND TRAILING EDGE ROTATING CYLINDER /
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EXPERIMENTAL STUDY OF MEAN FLOW CHARACTERISTICS OF SWIRLING JETS /
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EXPERIMENTAL STUDY OF FLOW CHARACTERISTICS OF ROUGHENED SURFACE AIRFOILS /
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HEAT TRANSFER ENHANCEMENT IN A PIPE FLOW USING A ROTATING TWISTED TAPE INSERT
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STUDY OF FLOW THROUGH A CIRCULAR PIPE AND CONSTRUCTION OF AN EXPERIMENTAL SET UP FOR THE STUDY /
त्वरित देखें
EXPERIMENTAL STUDY OF THE FLOW FIELD OF AN ANNULAR JET COALESCING AT THE EXIT