IGF::OT::IGF APPROACHES FOR WEIGHT PREDICTION, IN THE CONCEPTUAL DESIGN PHASE, TYPICALLY CONSIST OF PARAMET…

Public award description

IGF::OT::IGF APPROACHES FOR WEIGHT PREDICTION, IN THE CONCEPTUAL DESIGN PHASE, TYPICALLY CONSIST OF PARAMETRIC RELATIONS OR EMPIRICAL DATABASES. HISTORICAL DATABASES WORK REASONABLY WELL WHEN APPLIED TO EXISTING OR CONVENTIONAL DESIGNS, HOWEVER, THEY FAIL TO PREDICT ACCURATELY THE WEIGHTS AND LOADS ASSOCIATED WITH UNCONVENTIONAL DESIGNS (LIKE THE LOW BOOM FLIGHT DEMONSTRATOR). THERE EXISTS A NEED TO AUGMENT EXISTING HISTORICAL DATABASES WITH A PHYSICS-BASED METHODOLOGY/CAPABILITY FOR PREDICTING THE WEIGHTS AND LOADS OF UNCONVENTIONAL DESIGNS. IN THE CURRENT PROPOSAL, M4 ENGINEERING WILL CONTINUE TO STREAMLINE THE STRUCTURAL LAYOUT PROCESS, IMPROVE THE OVERALL USER EXPERIENCE, AND DEVELOP A COMPREHENSIVE SUITE OF CAPABILITIES IN AN EFFORT TO BUILD A COMPLETE WEIGHT STATEMENT FOR UNCONVENTIONAL (AND CONVENTIONAL) CONCEPTUAL WING AND FUSELAGE DESIGNS. THE MAIN GOAL FOR THIS EFFORT WILL BE TO DEVELOP A SOFTWARE TOOL CAPABLE OF GENERATING WEIGHT AND LOAD RESPONSES FOR UNCONVENTIONAL DESIGNS FROM PHYSICS-BASED STRUCTURAL ANALYSIS SIMULATIONS.