FIELD: aircraft engineering.
SUBSTANCE: claimed process comprises the selection performed by calculation of the ratios between the engine inner and outer outline lengths within over 1.41 or under 0.9 for all possible operating conditions of the aircraft.
EFFECT: ruled out the engine thrust loss, longer life of the aircraft airframe.
3 dwg, 2 tbl
Authors
Dates
2016-02-10—Published
2014-06-02—Filed