चैनल - GROUND SUPPORT EQUIPMENT OF ‘’ MIST X – 1’’ / :: Library Catalog

समान संसाधन: GROUND SUPPORT EQUIPMENT OF ‘’ MIST X – 1’’ /

त्वरित देखें
MAINTENANCE & SERVICE MANUAL OF MIST X -1 /
त्वरित देखें
DESIGN & FABRICATION OF WING CONTROLS,UNDERCARRIAGE AND SKIN OF HOME BUILT EXPERIMENTAL AIRCRAFT’’ MIST X-01’’ /
त्वरित देखें
DESIGN & DEVELOPMENT OF THRUST PROVIDER FOR A HOME BUILT AIRCRAFT (MIST-EXPERIMENTAL-1) /
त्वरित देखें
DESIGN & DEVELOPMENT OF STRUCTURE OF A PROTOTYPE AIRCRAFT MIST EXPERIMENTAL-1 / Refaty Munni, Najifa Tasnim & Asif Bin Hossain.
त्वरित देखें
DEVELOPMENT OF MICRO CONTROLLER BASED AVIONICS PACKAGE WITH REAL TIME FLIGHT VISUALIZATION EMERGENCY AUTO LANDING AND FLIGHT DATA RECORDER /
त्वरित देखें
DEVELOPMENT OF A PHASED OUT AIRCRAFT AS EDUCATIONAL AID /
त्वरित देखें
EFFECT OF MOMENTUM INJECTION ON THE PERFORMANCE OF AIRFOIL (MOVING SURFACE BOUNDARY LAYER CONTROL /
त्वरित देखें
IDENTIFICATION, INTEGRATION AND TESTING OF AUTOPILOT AND AVIONIC EQUIPMENT IN A FIXED WING (UNMANNED AERIAL VEHICLE) TARGET DRONE FOR TESTING AIR DEFENCE SYSTEM /
त्वरित देखें
STRESSES IN AN ANGLE PLY LAMINATED CANTILEVER UNDER TRANSVERSE LOADING /
त्वरित देखें
MANUFACTURE AND MISSION PERFORMANCE ANALYSIS OF SMALL UNMANNED AIRCRAFT’ /
त्वरित देखें
ANALYSIS AND INSTALLATION OF AVIONICS SYSTEM IN A SMALL UNMANNED AIRCRAFT /
त्वरित देखें
SCALAR FUNCTION FORMULATION FOR STRESS ANALYSIS OF BOUNDARY VALUE PROBLEMS POLAR AND CYLINDRICAL COORDINATE SYSTEM / Farhan Hasan Nuri, Md. Shoriful Islam .
त्वरित देखें
STRESSES IN AN ANGLE PLY LAMINATED CANTILEVER UNDER SHEAR LOADING / Roohany Mahmud .
त्वरित देखें
INVESTIGATION OF DRAG EFFECT OF AROFOIL SHAPED FUSELAGE UAV MODEL AND VISUALIZATION OF AIR FLOW / Captain Md. Ruhul Amin Noor, Flying Officer Syeda Lira Rayhan & Flying Officer Umme Laila Amin
त्वरित देखें
DESIGN PROTOTYPE PROPOSAL OF OPTICAL FIBER BASED AVIONICS DATA BUS FOR A SMALL AIRCRAFT / S.M. Easin Ankur, Faisal Ahmed & Akter Mahmud Nafi .
त्वरित देखें
DESIGN & MODELING OF RADAR CONTROL SYSTEM FOR DETECTING AIRCRAFT & MISSILE /
त्वरित देखें
STRESSES IN ANGEL PLAY LAMINATED CANTILEVER UNDER BENDING MOMENT /
त्वरित देखें
STUDY OF FLOW OVER A FANWING IN A SUBSONIC WIND TUNNEL / Sajida Akter Jahan, Sadia Kamal Mery, Tarek Zobaer.
त्वरित देखें
DESIGN AND FABRICATION OF A MICRO UAV WITH DEVELOPMENT OF ITS STRUCTURE, PROPULSION AND CONTROL SYSTEM / Md. Tauhid Rahman Evan, Mir Md. Al Kahman Tamal, Md. Jamal Mian
त्वरित देखें
DESIGN AND FABRICATION OF AIRFRAME STRUCTURE & CONTROLS OF UAV / Md. Fazlay Robbey, Md. Mukit Hasan, Saiful Islam .
त्वरित देखें
STUDY OF FLOW CHARACTERISTIC OF A CIRCULAR JET / Umama Sharah Taskia, Maliha Yelmahi, Fatema Tarannum & Afifa Muna.
त्वरित देखें
A STUDY OF IMPROVEMENTS ENGINES PERFORMANCE APPLYING INTERCHANGEABILITY ASSOCIATED WITH RAIN AND A NEW APPROACH OF GNESS BASED LANDING SYSTEM /
त्वरित देखें
REVIEW OF OPTICAL FIVER DATA BUS AND FLY- BY LIGHT CONCEPT IN AVIATION /
त्वरित देखें
COMPARATIVE STUDY OF SWIRL FLOW & JET FLOW /

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

विषय: Aeronautical Engineering.

लेखक: Saimun, Lt Zulfikar Hyder

त्वरित देखें
GROUND SUPPORT EQUIPMENT OF ‘’ MIST X – 1’’ /

लेखक: Lt Hamdi Hishan Ahmed Hushaya

त्वरित देखें
GROUND SUPPORT EQUIPMENT OF ‘’ MIST X – 1’’ /