FIELD: aviation; methods of protection of flying vehicle engines against foreign object ingestion. SUBSTANCE: zone where vortex flows are absent is determined above airfield. This zone is located between maximum altitude at which suction of foreign objects is started and maximum altitude at which vortex flows are formed. Engine air intake is placed in zone where vortex flows are absent. EFFECT: enhanced efficiency and safety of flights. 3 dwg
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Authors
Dates
2003-11-27—Published
2002-04-12—Filed