FLYING VEHICLE FUSELAGE Russian patent published in 1998 - IPC

FIELD: aeronautical engineering; transport facilities moving at subsonic speed. SUBSTANCE: flying vehicle fuselage includes frontal surface changing to tail section. frontal surface is engageable with maximum diameter of fuselage having form of straight round cone at angle r = k²v²/ω over entire circle from nose point to maximum diameter by radius r determined from formula γ,, where r is rounding-off radius of frontal surface, m; k is coefficient of increase of air flow velocity on surface of maximum diameter of fuselage; V is flight speed; m/s: ω is acceleration, m/sq.s γ is fuselage taper angle. EFFECT: enhanced reliability. 2 dwg