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Seoul National University Employs VABS for Helicopter Blade Optimisation

05 June 2018

AnalySwift has announced that Seoul National University is leveraging its VABS software to accelerate and optimise design of composite helicopter rotor blades and high aspect ratio wings.

Seoul National University has used VABS for a variety of structural optimisation projects in its Active Aeroelasticity and Rotorcraft Laboratory (AARL), which is part of the Department of Aerospace Engineering.

“We have worked with the Active Aeroelasticity and Rotorcraft Laboratory at Seoul National University for several years and we are pleased they selected VABS to be part of their toolset for simulation of composite rotor blades and other slender structures,” says Allan Wood, President and CEO of AnalySwift. “The AARL is involved in a variety of exciting research areas for which VABS can accelerate design by delivering accurate and efficient results.”

The AARL investigates aeroelastic phenomena occurring in aircraft and spacecraft, under the direction of Professor SangJoon Shin. Specifically, aeroelasticity examines interactions among the inertial, aerodynamic and elastic forces on the aerospace vehicles, which generate large deflections of the structures that may lead to destructive failures. Thus, precise prediction of the aeroelastic behaviours is required to prevent failure of the aerospace vehicles. Moreover, aeroservoelasticity seeks more comprehensive solutions where active devices or control surfaces alter coupled structural behaviours, and aerothermoelasticity investigates aeroelastic problems involving thermodyamic effects.

“The VABS program is a uniquely powerful tool for modelling composite blades and other slender structures, commonly called beams,” explains Dr Wenbin Yu, CTO of AnalySwift. “VABS reduces analysis time from hours to seconds by quickly and easily achieving the accuracy of detailed 3D FEA with the efficiency of simple engineering models. With VABS, engineers can calculate the most accurate, complete set of sectional properties such as torsional stiffness, shear stiffness, shear centre for composite beams made with arbitrary cross-section and arbitrary material. It can also predict accurate detailed stress distribution for composite beams, which are usually not possible with 3D FEA for realistic composite structures.”

Comprehensive analyses for rotorcrafts and high aspect-ratio wings are performed at AARL using commercial, open source and in-house codes for the geometrically exact beam theory where the one-dimensional beam and two-dimensional cross-sectional properties are used. Therefore, structural optimisation programs using VABS are frequently developed and used. Thanks to the powerful pre-post processing utility PreVABS, global optimisation framework using scripts written in other tools is easily constructed.

Two current projects being designed, in part, using VABS include an active helicopter rotor blade equipped with a trailing-edge flap, as well as a slender wing for human-powered aircraft.

In order to solve coupled problems regarding aerospace structures, researchers use computational structural dynamics (CSD) and computational fluid dynamics (CFD), and attempt to verify those with experimental correlations. Examples of the past and current research projects include:

  • fully coupled CSD/CFD analysis for flexible structures such as an insect-inspired flapping wing micro air vehicle using an enhanced structural element and Navier-Stokes equation;
  • coupled aeroelastic dynamic analysis with control for unmanned aerial and space launch vehicles;
  • nonlinear flutter prediction for flexible aircrafts;
  • acoustic analysis for high speed vehicle applications; and
  • multidisciplinary design optimisation of rotorcrafts and active rotor blades such as active trailing-edge flaps.

Developed at Georgia Institute of Technology (Georgia Tech) and Utah State University, VABS is available through AnalySwift.






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