चैनल - COGNITIVE STUDY ON RADAR PERFORMANCE ANALYSIS WITH THE EFFECT OF SENSITIVITY TIME CONTROL (STC) / :: Library Catalog

समान संसाधन: COGNITIVE STUDY ON RADAR PERFORMANCE ANALYSIS WITH THE EFFECT OF SENSITIVITY TIME CONTROL (STC) /

त्वरित देखें
EFFECT OF ROTATING CYLINDER ON THE PERFORMANCE OF SYMMETRIC AIRFOIL: “AN EXPERIMENTAL STUDY /
त्वरित देखें
ANALYSIS OF MOVING TARGET RADAR CROSS-SECTION AND STUDY ON ELECTROMAGNETIC RADAR SIGNAL PROCESSING TO DEVELOP EFFICIENT TARGET INDICATOR (MTI) RADAR SYSTEM /
त्वरित देखें
DESIGN & MODELING OF RADAR CONTROL SYSTEM FOR DETECTING AIRCRAFT & MISSILE /
त्वरित देखें
DESIGN & DEVELOPMENT OF RADAR COOLANT MONITORING , ALARMING AND CONTROLLING SYSTEM /
त्वरित देखें
EFFECT OF MOMENTUM INJECTION ON THE PERFORMANCE OF AIRFOIL (MOVING SURFACE BOUNDARY LAYER CONTROL /
त्वरित देखें
STUDY MEASUREMENT AND REDUCTION OF RADAR CROSS SECTION (RCS) /
त्वरित देखें
DESIGN DEVELOPMENT OF WEAPON CONTROL SYSTEM TO ACCOMMODATE GUIDED AMMUNITION AND ROCKET POD /
त्वरित देखें
STUDY AND DESIGNING OF MICRO CONTROLLER BASED TEMPERATURE SENSING SYSTEM ALONG WITH GLOBAL SYSTEM FOR MOBILE INTERFACE AND ALARM MECHANISM TO BE USED IN EFFERENT TEMPERATURE SENSITIVE STOREHOUSES /
त्वरित देखें
DEVELOPMENT OF AN OPEN SYSTEM ARCHITECTURE USING REAL-TIME DATA ACQUISITION AND TELEMETRY FOR EFFECTIVE FLIGHT DATA VISUALIZATION AND ANALYSIS /
त्वरित देखें
STUDY ON DESIGNING OF TRANSMISSION SECTION OF A LOW COST PHASED ARRAY RADAR SYSTEM /
त्वरित देखें
STUDY OF FAULT TOLERANT FLIGHT CONTROL SYSTEM /
त्वरित देखें
STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY LAYER CONTROL ( MSBC) ON SINGLE & DOUBLE CYLINDER CONFIGURATION NACA 23018 AIRFOIL /
त्वरित देखें
COMPARATIVE STUDY OF CIRCULAR PLANE & SWIRLING JET /
त्वरित देखें
STUDY ON DESIGNING OF A RECEIVER SECTION OF A LOW COST PHASED ARRAY RADAR SYSTEM /
त्वरित देखें
DEVELOPMENT OF AN EXPERIMENTAL SETUP FOR ANALYZING THE INFLUENCE OF MAGNUS EFFECT ON THE PERFORMANCE OF AIRFOIL /
त्वरित देखें
INVESTIGATION OF THE EFFECT OF DIFFERENT AIRFOIL SHAPED FUSELAGE ON THE PERFORMANCE OF AN UNMANNED AIR VEHICLE /
त्वरित देखें
DEVELOPMENT OF MICRO CONTROLLER BASED AVIONICS PACKAGE WITH REAL TIME FLIGHT VISUALIZATION EMERGENCY AUTO LANDING AND FLIGHT DATA RECORDER /
त्वरित देखें
ANALYSIS OF RADAR CROSS SECTION (RCS) OF DIFFERENT SHAPE OF TARGETS USING MICROSTRIP ANTENNA IN ORDER TO DESIGN & FABRICATE A PROTOTYPE OF LOW COST PHASED ARRAY RADAR /
त्वरित देखें
STUDY AND COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS AND IMPROVED PERFORMANCE OF NACA 0015 AIRFOIL WITH BLEED /
त्वरित देखें
STUDY OF MOMENTUM INJENCTION: EFFECT OF CLEARENCE BETWEEN ROTATING CYLINDER AND GROOVED AIRFOIL /
त्वरित देखें
"INFLUENCE OF SURFACE MODIFICATION ON THE LIFT-DRAG CHARACTERISTICS OF NACA 0012 AIRFOIL" /
त्वरित देखें
STUDY OF FAULT TOLERANCE OF A FLIGHT CONTROL SYSTEM ACTUATOR IN FLY-BY-WIRE SYSTEM /
त्वरित देखें
COMPARATIVE STUDY OF AIRCRAFT APPROACH AND LANDING PERFORMANCE USING ILS, MLS AND GLS /
त्वरित देखें
A FRAMEWORK FOR REAL-TIME HUMAN DETECTION AND AUTONOMOUS RESPONSE IN SWARM UAV-BASED SURVEILLANCE /

विषय: Aeronautical Engineering.

विषय: This Thesis Paper of AE in B.Sc. Program.

लेखक: Mim, Sherajul Mamun

त्वरित देखें
COGNITIVE STUDY ON RADAR PERFORMANCE ANALYSIS WITH THE EFFECT OF SENSITIVITY TIME CONTROL (STC) /

लेखक: Haque, A.K.M. Ahadul

त्वरित देखें
COGNITIVE STUDY ON RADAR PERFORMANCE ANALYSIS WITH THE EFFECT OF SENSITIVITY TIME CONTROL (STC) /