STUDY OF CIRCULAR SWIRLING JET /

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Bibliografski detalji
Glavni autor:	Rahman, Md. Rafi ur
Autor kompanije:	Supervised by Dr. M. A. Taher Ali (Professor, Dept. of AE, MIST.)
Daljnji autori:	Nayem, Noor Mohammad, Nayeem, Muhammed Hasnain Kabir
Format:	Knjiga
Jezik:	engleski
Izdano:	Dhaka : AE DEPT. MIST, c2018.
Teme:	Aeronautical Engineering This Thesis Paper of AE in B.Sc. Program.
Oznake:	Dodaj oznaku Bez oznaka, Budi prvi tko označuje ovaj zapis!

Slični predmeti: STUDY OF CIRCULAR SWIRLING JET /

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COMPARATIVE STUDY OF CIRCULAR PLANE & SWIRLING JET /
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COMPARATIVE STUDY OF SWIRL FLOW & JET FLOW /
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EXPERIMENTAL STUDY OF MEAN FLOW CHARACTERISTICS OF SWIRLING JETS /
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A STUDY OF FLOW THROUGH CIRCULAR PIPE /
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EXPERIMENTAL STUDY OF CO-ROTATING SWIRLING JETS /
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STUDY OF FLOW CHARACTERISTIC OF A CIRCULAR JET / Umama Sharah Taskia, Maliha Yelmahi, Fatema Tarannum & Afifa Muna.
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A STUDY OF FLOW THROUGH CIRCULAR PIPE /
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STUDY OF FLOW BEHIND A CIRCULAR CYLINDER AND AN AIROFOIL /
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A COMPREHENSIVE STUDY OF FLOW THROUGH CIRCULAR PIPE /
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EXPERIMENTAL STUDY OF THE FLOW FIELD OF AN ANNULAR JET COALESCING AT THE EXIT /
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APPLICATION OF SCALAR FUNCTION FORMULATION TO A SEMI CIRCULAR DEEP ARCH /
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JET IMPINGEMENT COOLING OVER A FLAT PLATE /
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NUMERICAL INVESTIGATION OF LIFT AUGMENTATION WITH CO-FLOW JET AIRFOIL /
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A STUDY OF STATIC EXTENDED TRAILING EDGE FOR LIFT ENHANCEMENT /
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DESIGN OF A FIXED WING JET PROPULSION POWERED UNMANNED AERIAL VEHICLE (UAV) TARGET DRONE /
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EXPERIMENTAL STUDY OF FLOW VELOCITY AND DIRECTION AROUND NACA 0012 & NACA 0015 AIRFOIL /
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CFD ANALYSIS OF COMBUSTION CHARACTERISTICS FOR CAN-SWIRL TYPE COMBUSTION WITH CORRUGATION ON THE SURFACE /
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SUPERSONIC FLOW CONTROL IN COMPRESSION CORNER BY MICRO-VORTEX GENERATOR AND MICRO-JET /
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THE EXPERIMENTAL STUDY OF THE AERODYNAMIC CHARACTERISTICS OF THE AIRFOIL OF FOUGA MAGISTER 170 /
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STUDY ON DIFFERENT KIND OF BOMB DEPLOYMENT SYSTEM AND ARMAMENT SEQUENCING OF AN AIRCRAFT /
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STUDY ON MECHANICAL BEHAVIOR OF SISAL AND BANANA FIBER REINFORCED POLYMER MATRIX COMPOSITES /
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EFFECT OF CROSS –SECTIONAL SHAPES ON FREE JET CHARACTERIZATION NUMERICAL AND EXPERIMENTAL INVESTIGATION FEASIBLE AND PERFORMANCE OF DIFFERENT EXHAUST GEOMETRY /
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MODIFICATION OF A TURBO-JET ENGINE (F-7 ENGINE) AS A TRAINING AID / Flg offr A.K.M.Tajul Islam, Flg offr Md. Sayed Jaber, Flg offr B.M.Anisuzzaman
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STUDY OF FAULT TOLERANT FLIGHT CONTROL SYSTEM /