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Published byEdwin Shawn Bates Modified over 9 years ago
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Scientific Programmes Committee Centre for Aerospace Systems Design & Engineering SK Sane Department of Aerospace Engineering Indian Institute of Technology, Mumbai www.casde.iitb.ac.in/MDO/modules/Sanghi-Sane-ICAS-593.pdf July 5, 2003 Engine Optimization
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Airframe Aerodynamics, Structures, Controls, Weight etc MDO Transport Aircraft System {Design Variables} Mission Profile Specifications Optimizers RSM + Box DACE + EGO Installed off-Design Performance T, mf, ma, ΔD = f (M, H, PLA) Design Point Engine Envelope Propulsion System Weight
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Tasks for Next Six Months Improved Engine Envelope and Weight Module Verification of Code throughout the Design Space Application of DACE Models to Replace RSM
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