Documenti analoghi: DESIGN AND PARAMETRIC ANALYSIS OF H-PLANE HORN & MICROSTRIP PATCH ANTENNA AT X-BAND FOR INTERFERENCE SUPPERESION /
- INNOVATIVE DESIGN AND EVALUATION OF MICROSTRIP PATCH ANTENNAS FOR 5G COMMUNICATION IN MILLIMETER WAVE BAND /
- DESIGN OF A DUAL-BAND MICROSTRIP PATCH ANTENNA WITH ENHANCED BANDWIDTH AND GAIN FOR 5G APPLICATIONS /
- DESIGN AND PERFORMANCE ANALYSIS OF A MICROSTRIP PATCH ANTENNA FOR GNSS APPLICATIONS /
- BANDWIDTH ENHANCEMENT AND PERFORMANCE ANALYSIS OF 6G V-BAND MICROSTRIP PATCH ANTENNA ESTIMATING ATMOSPHERIC AND PATH LOSS /
- DESIGN OF A MICROSTRIP PATCH ANTENNA IN A SILICON SUBSTRATE USING HFSS
- COMPREHENSIVE DESIGN AND REALIZATION OF DUAL-BAND, KU-BAND AND X-BAND REFLECTARRAY ANTENNAS USING COMPACT SPLIT-RING UNIT CELLS /
Soggetto: Aeronautical Engineering
- COMPARATIVE STUDY OF SWIRL FLOW & JET FLOW /
- COMPARATIVE STUDY OF AIRCRAFT APPROACH AND LANDING PERFORMANCE USING ILS, MLS AND GLS /
- MANUFACTURE AND MISSION PERFORMANCE ANALYSIS OF SMALL UNMANNED AIRCRAFT’ /
- A COMPARISON OF EXPERIMENTAL WITH SIMULATION EFFECTIVE OF NACA 0012 AIRFOIL WITH BARE /
- EFFECT OF CROSS –SECTIONAL SHAPES ON FREE JET CHARACTERIZATION NUMERICAL AND EXPERIMENTAL INVESTIGATION FEASIBLE AND PERFORMANCE OF DIFFERENT EXHAUST GEOMETRY /
- PROPERTIES OF NATURAL POLYMER MATRIX COMPOSITE WITH VARIOUS FIBER ORIENTATIONS /
Soggetto: This Thesis Paper of AE in BSc Program.
- DIFFERENTIALLY PRIVATE MULTY-STAGE FLIGHT DELAY PREDICTION NETWORK (DP-MSFDPN): A PRIVACY-PRESERVING THREE-STAGE TEMPORAL CONVOLUTION FRAMEWORK /
- ADAPTIVE DRONE PATH OPTIMIZATION USING D*LITE, NONLINEAR MODEL PREDICTIVE CONTROL AND B-SPLINE TRAJECTORY PLANNING /
- DESIGN AND IMPLEMENTATION OF A COORDINATE UAV SWARM FOR LONG RANGE OPERATIONS /
- DESIGN AND FABRICATION ON VACUUM ASSISTED INFUSIUN MOLDING SETUP FOR FABRICATION OF FLAT AND CURVED COMPOSITE PANELS /
- SYNTHESIS AND CHARACTERIZATION OF JUTE-DERIVED CARBON MATERIALS FOR ADVANCED COMPOSITE AND WATER FILTRATION APPLICATIONS /
- DESIGN AND COMPUTATIONAL ANALYSIS OF SUBSONIC LOITER MUNITION'S WING USING DIFFERENT AIRFOIL SECTION /
Autore: Mashunur Rahman, Mohammad
Autore: Supervised by Mahbuba Ferdous
- DEVELOPMENT OF PROGAMMABLE HOT WIRE CNC MACHINE FOR AEROSTRUCTURE FABRICATION /
- MULTI-PHYSICS ANALYSIS OF FIBER-REINFORCED ANISOTROPIC COMPOSITES UNDER ELECTRO-THERMAL BOUNDARY CONDITIONS /
- COGNITIVE STUDY ON RADAR PERFORMANCE ANALYSIS WITH THE EFFECT OF SENSITIVITY TIME CONTROL (STC) /
- DEVELOPMENT AND TESTING OF A LOW POWERED COST-EFFECTIVE FREQUENCY MODULATOR FOR APPLICATIONS IN RE TRANSMISSION /
- THERMO-MECHANICAL ANALYSIS OF AIRCRAFT STRUCTURES REINFORCED WITH STIFFENERS /
- DESIGN AND PARAMETRIC ANALYSIS OF H-PLANE HORN & MICROSTRIP PATCH ANTENNA AT X-BAND FOR INTERFERENCE SUPPERESION /