Transcript MULTIDISCIPLINARY OPTIMIZATION OF PROPULSION SYSTEM …

Engine Optimization
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
Airframe Aerodynamics,
Structures, Controls,
Weight etc
Mission Profile Specifications
MDO Transport Aircraft
System
{Design Variables}
Installed off-Design Performance
T, mf, ma, ΔD = f (M, H, PLA)
Design Point Engine Envelope
Propulsion System Weight
Optimizers
RSM + Box
DACE + EGO
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