FIELD: aircraft engineering.
SUBSTANCE: aircraft comprises wing connected with fuselage with its nose and tail that feature round cross-section. Aircraft tail is equipped with engine with nacelle and two air intakes arranged behind the recess. Said recess is confined by first flat site and two second sites arranged between said first site and engine air intakes. Second sites are connected at an angle to each other along the rib extending nearby aircraft mirror plane.
EFFECT: decreased irregularity of supersonic airflow in air intakes.
11 cl, 15 dwg
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Authors
Dates
2014-05-27—Published
2012-11-20—Filed