Canales - DEVELOPMENT OF AIRCRAFT SYSTEM DEMONSTRATOR: FOUGA CM170 MAGISTER AIRCRAFT / :: Library Catalog

Ejemplares similares: DEVELOPMENT OF AIRCRAFT SYSTEM DEMONSTRATOR: FOUGA CM170 MAGISTER AIRCRAFT /

Tópico: Thesis Paper of AE in B.Sc Prog.

Vista rápida
COMPARATIVE STUDY OF SWIRL FLOW & JET FLOW /
Vista rápida
COMPARATIVE STUDY OF AIRCRAFT APPROACH AND LANDING PERFORMANCE USING ILS, MLS AND GLS /
Vista rápida
MANUFACTURE AND MISSION PERFORMANCE ANALYSIS OF SMALL UNMANNED AIRCRAFT’ /
Vista rápida
A COMPARISON OF EXPERIMENTAL WITH SIMULATION EFFECTIVE OF NACA 0012 AIRFOIL WITH BARE /
Vista rápida
EFFECT OF CROSS –SECTIONAL SHAPES ON FREE JET CHARACTERIZATION NUMERICAL AND EXPERIMENTAL INVESTIGATION FEASIBLE AND PERFORMANCE OF DIFFERENT EXHAUST GEOMETRY /
Vista rápida
PROPERTIES OF NATURAL POLYMER MATRIX COMPOSITE WITH VARIOUS FIBER ORIENTATIONS /
Vista rápida
A COMPREHENSIVE STUDY OF FLOW THROUGH CIRCULAR PIPE /
Vista rápida
MODELING AND SIMULATION OF LONGITUDINAL AUTOPILOT FOR GENERAL AVIATION AIRCRAFT /
Vista rápida
DEVELOPMENT OF A PHASED OUT AIRCRAFT AS EDUCATIONAL AID /
Vista rápida
MACHINABILITY OF POLYMER MATRIX COMPOSITES (PMC)-A REVIEW OF CURRENT STATUS AND FUTURE PROSPECTS /
Vista rápida
ANALYSIS AND INSTALLATION OF AVIONICS SYSTEM IN A SMALL UNMANNED AIRCRAFT /
Vista rápida
STRUCTURAL ANALYSIS OF AIR CRAFT WINGS WITH VARIOUS CONDITIONS /
Vista rápida
COMPARATIVE AND ASSESSMENT OF VARIOUS TURBULENCE MODELS AND IMPROVED PERFORMANCE OF NACA 0010 AIRFOIL WITH MSBLC /
Vista rápida
COMPARATIVE ASSESSMENT OF TURBULENCE OF IMPROVED PERFORMANCE OF NAC 0012 AIRFOIL WITH MSBLC /
Vista rápida
DESIGN OF A CLOSED LOOP SUBSONIC WIND TUNNEL /
Vista rápida
DESIGN AND FABRICATION OF TSVU (TRI COPTER SHAPED VTOL UAV) /
Vista rápida
EFFECT OF ROTATING CYLINDER ON THE PERFORMANCE OF SYMMETRIC AIRFOIL: “AN EXPERIMENTAL STUDY /
Vista rápida
COMPARATIVE STUDY OF CIRCULAR PLANE & SWIRLING JET /
Vista rápida
STUDY OF FLIGHT DATA RECORDER SAFETY AND SURVIVAL SYSTEM /
Vista rápida
STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY LAYER CONTROL ( MSBC) ON SINGLE & DOUBLE CYLINDER CONFIGURATION NACA 23018 AIRFOIL /
Vista rápida
AERODYNAMICS PERFORMANCE ANALYSIS OF 2D AIRFOIL/ NACA 4418 INCORPORATING WITH ROTATING CYLINDER /
Vista rápida
LARGE DEFECTION ANALYSIS OF AN AIRCRAFT WING WITH ELLIPTICAL LIFT DISTRIBUTION AT DIFFERENT FLIGHT CONDITION /
Vista rápida
STUDY AND COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS BETWEEN DIFFERENT CONFIGURATIONS OF THREE DIMENSIONAL MODELS OF NACA 4412 AIRFOIL /
Vista rápida
EXPERIMENTAL STUDY OF FLOW CHARACTERISTICS OF ROUGHENED SURFACE AIRFOILS /

Tópico: Aeronautical Engineering.

Autor: Capt, Arif Md. Amirul Abrar

Vista rápida
DEVELOPMENT OF AIRCRAFT SYSTEM DEMONSTRATOR: FOUGA CM170 MAGISTER AIRCRAFT / Capt Arif Md. Amirul Abrar, Capt A Ashigur Rahman Sany, Hannanur Rashid Saddam.

Autor: Capt Hannanur Rashid Saddam

Vista rápida
DEVELOPMENT OF AIRCRAFT SYSTEM DEMONSTRATOR: FOUGA CM170 MAGISTER AIRCRAFT / Capt Arif Md. Amirul Abrar, Capt A Ashigur Rahman Sany, Hannanur Rashid Saddam.