FIELD: aviation.
SUBSTANCE: proposed aircraft has flat fuselage and turbo-jet engines. Fuselage is elongated along longitudinal axis and is provided with seats in front of which passengers bow and height of passage is sufficient for standing upright. Turbo-jet engines suck air flow above fuselage. Vertical walls mounted over fuselage edges pass over inclined trajectory to longitudinal axis without fully closing the inner cavity to upper point.
EFFECT: decreased drag.
3 dwg
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