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title: Multidisciplinary analysis and optimization
Multidisciplinary design and optimization of expendable launch vehicle for microsatellite missions
Multidisciplinary optimisation needs to be an integral part of analysis and design process. The successful optimisation results allowed to meet the
...Aerodynamic wing shape optimization based on the computational design framework CEASIOM
A collaborative design environment is needed for multidisciplinary design optimization (MDO) process, based
...Proof-of-concept analysis of a supplemental solar power system for aircraft
Coupling of static and dynamic fuselage design
– A fuselage barrel was computed statically and dynamically using finite element methods. Static analysis was conducted using a global/local
...Design-airworthiness integration method for general aviation aircraft during early development stage
A new design and optimization process is proposed that logically includes the airworthiness regulations as design
...Uncertainty-based MDO for aircraft conceptual design
Development of an improved framework for the conceptual design of a rotorcraft
Common computational model for coupling panel method with finite element method
Comprehensive approach to comparative efficiency evaluation of HPS for helicopters
– The purpose of the work is to carry out analysis of the possibilities and estimation of
...A review of hybrid-electric energy management and its inclusion in vehicle sizing
Aircraft design using a variable density model
Optimization algorithms based on fully-stressed design philosophy, sensitivity coefficients, and employing material density as a design variable
...Wing shaping concepts using distributed propulsion
– Multidisciplinary analysis and trajectory optimization are used to evaluate the mission
...Artificial neural networks to predict aerodynamic coefficients of transport airplanes
Morphing wing with skin discontinuity – kinematic concept
Multidisciplinary numerical optimization will be used to determine control allocation for wing segments rotation. Wing
...Modeling of CPACS-based fuselage structures using Python