A METHOD FOR PROVIDING AN INTEGRATED ENGINEERING ANALYSIS PROCESS WITH A SOLUTION FEEDBACK FOR AN AIRCRAFT ENGINE DESIGN.

摘要

The Invention relates to an integrated engineering analysis system that determrnes at least one final output value in response to at least one initial input value. A first subprocesses provides at least one output value in response to the initial input value. A plurality of subprocesses provide a plurality of output values in response to the output values of the first subprocess. The plurality of output values and the output value of the first subprocess are inputted into at least one of the plurality of subprocesses. A command code executes each of the plurality of subprocesses in response to the output values and determines which one of the plurality of subprocesses to run and a final subprocess provides a final output. The fmal output is the result of a plurality of calculations executed by the plurality of subprocesses and the command code compares the final output with the initial input.