Những quyển sách tương tự: ACTIVE CONTROL OF FLOW SEPARATION OVER SUPERCRITICAL AIRFOIL USING SYNTHETIC JET /
- MACHINE LEARNING APPROACH TO SHOCK DETECTION IN COMPRESSIBLE FLOW OVER A WEDGE /
- STUDY OF IMPACT OF JET ON DIFFERENT VANES FOR MEASURING FLOW RATE AND IMPACT FORCE /
- SYNERGISTIC FLOW CONTROL: INGRATION OF DYNAMIC VORTEX GENERATORS AND VARYING DIMPLE GEOMETRIES FOR ENHANCED AERODYNAMIC CHARACTERISTICS FOR NACA 2412 AIRFOIL /
- NUMERICAL INVESTIGATION OF LIFT AUGMENTATION WITH CO-FLOW JET AIRFOIL /
- DEVELOP A CUT VIEW MODEL OF JET ENGINE /
- Active Control of Noise and Vibration : Volume I /
Đề tài: Mechanical Engineering.
- AN EXPERIMENTAL ANALYSIS OF THE THERMAL CONDUCTIVITY AND STABILITY OF CuO-TiO2-ZnO TRIHYBRID NANOFLUID /
- THERMAL BEHAVIOUR OF SN42-BI58 SOLDER ALLOY AND ITS INTERFACIAL CHARACTERISTICS WITH MILD STEEL SUBSTRATES: A SEMI METALLIC BRAKE PAD BACKING PLATE CASE STUDY /
- DEVELOPMENT OF BULLET PROTECTIVE PANEL FROM RECYCLED TIRES /
- MODELING AND SIMULATION OF PRESSURE WAVE PROPAGATION OF AN AUTOMOTIVE EXPLOSION ENGINE MUFFLER USING COMSOL MULTI PHYSICS SOFTWARE /
- STUDY OF TWO PHASE LOOP THERMOSYPHON BY USING VARIOUS EVAPORATOR SURFACE GEOMETRIES WITH DIFFERENT WORKING FLUIDS /
- STUDY ON PERFORMANCE CHARACTERISTICS OF CENTRIFUGAL PUMP AND CONSTRUCTION OF AN EXPERIMENTAL SET UP FOR THE STUDY /
Đề tài: This Thesis Paper of ME in B.Sc. Program.
- DEVELOP A CUT VIEW MODEL OF JET ENGINE /
- STRUCTURAL DESIGN ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE /
- DETERMINATION OF CRITICAL SPEED OF A SHAFT /
- DESIGN AND FABRICATION OF MODEL SURFACE TO SURFACE MISSILE LAUNCHING SYSTEM /
- DESIGN AND FABRICATION OF A MODEL SURFACE TO SURFACE MISSILE WITH MOTION CONTROL SYSTEM RUN BY COST-EFFECTIVE SOLID PROPELLANT /
- DESIGN AND FABRICATION OF A REMOTELY OPERATED UNMANNED COMBAT VEHICLE /