FIELD: aviation. SUBSTANCE: some aircraft land on runway during some periods of 24-hour cycle of airfield operation at presence of downwind component of wind velocity vector through entry corridor directed to arrival airfield; angular range ϕ between axis of runway and axis of entry corridor of aircraft is equal to v= ± 0,38π; take-off is effected in direction of downwind component of wind velocity vector at similar angular range between direction of axis of runway and direction of axis of exit corridor. EFFECT: enhanced reliability. 14 dwg
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Authors
Dates
1995-07-09—Published
1994-01-31—Filed