| 摘要 |
FIELD: aircraft engineering.SUBSTANCE: invention relates to aircraft engineering. Method of engine arrangement on “flying wing” type aircraft consists in fact, that engine nacelle (1) is installed in wing (2) trailing-edge assembly so, that gap between engine nacelle (1) lower point and wing (2) surface is (0.37-0.41)D, where D is air intake inlet cross-section inner diameter.EFFECT: invention increases aerodynamic quality.1 cl, 1 tbl, 6 dwg |
