An Unmanned Aerial Vehicle blimp kind
prototype for stable environmental conditions is shown in
this paper. The lift, drag, weight, and thrust parameters are
analyzed on the basis of the Archimedes principle, Bernoulli
and continuity equations, and fluid simulations for different
conditions (low-speed wind and absence of turbulence). The
calculated push force (lift) is the minimum value to produce
sustentation considering the overall mass of the aircraft. On
the other hand, the drag parameter was analyzed using the
fluid simulation to visualize the drag force.International Journal of Mechanical Engineering and Robotics Researchdoi: 10.18178/ijmerr.7.2.197-20
