Zobrazeno 1 - 10
of 17
pro vyhledávání: '"Shiva Prasad U"'
Publikováno v:
Graduate Research in Engineering and Technology. :1-4
Despite all the other rocket motors on the market such as solid and liquid. A historically failed motor was in the market which was handicapped in performance but now with technological development in the previous years, hybrid rocket motor is the mo
Publikováno v:
Graduate Research in Engineering and Technology. :5-9
The aerodynamic coefficients and flow surrounding a canard missile design were predicted using viscous computational fluid dynamics simulation. The computations were performed at speeds between 1.5 and 3.0. High-speed flight is possible with canard d
Publikováno v:
Graduate Research in Engineering and Technology. :45-48
The solid rocket motor upper stage for a space launch vehicle is a more efficient propulsion technology than the liquid rocket motor upper stage. Its grain design has the potential to be crucial in terms of lowering inert mass by adopting improved vo
Publikováno v:
Graduate Research in Engineering and Technology. :105-111
The Primarily focus on Graphene Aerogel, its synthesis and structural integrity together with high electrical conduction. Graphene could be a new nanocarbon that has, single-, bi- or few- layers of carbon atoms forming membered rings. Mechanically po
Publikováno v:
Graduate Research in Engineering and Technology. :133-139
Blended wing body is a fixed wing aircraft which are smoothly blended together with no clear dividing line and no distinct wings also be given a wide Aerofoil shaped body. The future transportation is of aircrafts will incline towards the aerodynamic
Publikováno v:
Graduate Research in Engineering and Technology. :8-13
High Altitude Long Endurance Unmanned Aerial Vehicles (HALE UAVs) could provide an improved service and/or flexibility at a reduced cost over existing systems for a vast number of civil patrol and surveillance applications. This document looks into t
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Akademický článek
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