Loads and Structural Optimization Process for Composite Long Range Transport Aircraft Configuration
Published: Jun 24, 2018
Abstract
Background: The consideration of composite design in an early design phase has become more and more necessary in aircraft design. In the scope of multidisciplinary optimisation, a composite aeroelastic reference model is often desired to investigate multidisciplinary effects on a near-industrial application.
Objective: The aim is to generate a benchmark aeroelastic model by developing a robust design process for composite...
Paper Details
Title
Loads and Structural Optimization Process for Composite Long Range Transport Aircraft Configuration
Published Date
Jun 24, 2018
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