The design and manufacture of a remotely piloted aircraft
Journal Title: INCAS BULLETIN - Year 2011, Vol 3, Issue 2
Abstract
The article is a compilation of data regarding the process of designing an UAV wing, generally speaking, and an iteration of the stress calculations made during the research. Therefore, we use the best materials and a design that fits the necessities and requirements of such an airplane. The purpose of the UAV is to have a precise goal, namely to be used by the authorities for the people. Example: flying at low height for the surveillance of a large forest fire or a highway, or even for collecting data regarding the air quality and the percentage of noxious particles in different urban and nonurban areas.
Authors and Affiliations
Cosmin PESCARUS
[b]Profiles with Coanda effect, necessaries to wind turbines[/b]
The air flow separation around profiles and the wind turbine rotor vibration leading to the blade breaking is a well known phenomenon based on which the present work is conceived. The paper is focused on theoretic and ex...
ELIE CARAFOLI, WIDE INTERNATIONAL ACKNOWLEDGEMENT
Analysis of isogrid reinforced cylindrical vessels in the case of axially symmetric buckling
Isogrid structures are a configuration of stiffeners of different sections, which make up a lattice placed on thin plates, with the aim of increasing the buckling factor of the overall structure. Because of the major ben...
Professor Ion Stroescu’s role to the construction of aerodynamic wind tunnels
Present and future of aircraft carriers as a floating diplomatic and military means of deterrence
The aircraft carrier is the most capable offshore military warship the mankind has ever build and is considered as a symbol of the absolute navy and national strenght. Construction of an aircraft carrier is having a grea...