Four Lycoming 390X (840 hp total) on a experimental aircraft?
main concern @ bottom of brief exp. aircraft description:
(4) io-390x----8 pass----all metal-----high wing (2engines per wing)-----constant speed propellers-----retractable land gear-----bede's honeycomb panels-----bede's tubular wing spar-----2 air cond.-----top notch inst. , avionics , safety devices------custom leather interior-----very high lifting capability-----yokes----5 ft wide fuselage-----
please give me rough estimate have me dreaming until buy rds aircraft design software...
wing design should use?
how weight able lift (pass , cargo)?
how fast go (never exceed speed)?
main concerns have?
suggest?
my main concern @ bottom of brief exp. aircraft description: (4) io-390x----8 pass----all metal-----high wing (2engines per wing)-----constant speed propellers-----retractable land gear-----bede's honeycomb panels-----bede's tubular wing spar-----2 air cond.-----top notch inst. , avionics , safety...
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