cranfield0047

analysi low aspect ratio aircraft structur two method present analysi complex lowaspect ratio aircraft structur method provid arbitrari extern load gener respect orient structur member permit arbitrari boundari condit purpos analysi structur ideal network flexur member interconnect torsion box first method set linear equat obtain express boundari condit member deflect equat equilibrium requir slope compat relationship term deflect intern forc solut deflect intern forc form product invers structur matrix column matrix load function second method condit given boundari assembl column matrix transfer step bystep fashion entir structur opposit boundari transfer accomplish success multipl squar matric compos independ differ transfer rang final oper invers rel small matrix provid solut unknown boundari condit comparison theoret result experiment data electr analog solut favor