Published: 14 Apr 2026
Penn State Vertical Lift Research Center of Excellence is
pushing the boundaries of composite rotorcraft blade development by advancing
the iVABS framework toward a true design-to-production workflow. The initiative
focuses on embedding manufacturing constraints directly into the early-stage
design process, an area historically overlooked in simulation-driven composite
development.
Penn State has been participating in its
Academic Partner Program (APP), and have been using AnalySwift s VABS
simulation software as well as the open source iVABS tool to improve the
manufacturability of composite rotor blades used for helicopters, air mobility,
and other rotorcraft.
AnalySwift, LLC., is a provider of efficient high-fidelity
modeling software for composites. The work is part of the Penn State
Vertical Lift Research Center of Excellence (VLRCOE), a premier research and
education hub at Penn State dedicated to advancing vertical lift technologies, such
as helicopters, drones, and VTOL systems, in key areas like aeromechanics,
flight dynamics, propulsion, acoustics, and survivability.
The APP offers participating universities no-cost licenses
of engineering software programs VABS and SwiftComp so students, researchers,
and faculty can leverage the tools in their academic research.
The VABS program is a general-purpose
cross-sectional analysis tool for predicting structural beam properties and
recovering 3D stresses, strains, and strengths of slender composite
structures. It is a powerful tool for modeling composite rotorcraft
(helicopter, air mobility, unmanned aerial vehicles) and wind turbine rotor
blades, as well as other slender composite structures, such as propellers,
landing gear, and high-aspect ratio wings.
iVABS is a VABS-based structural design
framework, enables VABS for design and optimization, parametric
studies, and uncertainty quantifications in a user-friendly way. This framework
bundles PreVABS, VABS, GEBT, and third-party tool Dakota, along with Python for
integration among these codes and other codes.
We are excited by the work being done by the VLRCOE at Penn State and pleased they have found VABS helpful as they further advance the iVABS platform, said Allan Wood, president & CEO of AnalySwift. As a versatile cross sectional analysis tool, VABS delivers high-fidelity results early on to help computationally resolve engineering challenges, reduce trial and errors, and arrive at the best solution more quickly.
Full-Scale Composite Rotor Blade Optimization with Manufacture
Awareness
The optimization of rotor blade design plays a critical
role in improving overall rotorcraft performance, said Jiwoo Song, who is pursuing a PhD degree in aerospace engineering at Penn State. Recent
advancements in computational toolchains, such as iVABS, enable rapid
exploration of design spaces while satisfying prescribed performance
objectives. The goal of the project is to achieve a design-to-production capability
by developing a drastically more manufacturing-aware iVABS blade design
framework. Looking ahead, this project aims to move beyond virtual optimization
into physical realization, with plans to fabricate a composite rotor blade in
collaboration with the Penn State Applied Research Laboratory, validating the
computational design process through experimental testing.
The VABS software has been central to my research in rotor
blade structural optimization,
continued Song. Its high-fidelity cross-sectional analysis capability
allows me to rapidly compute stiffness, mass, and coupling properties for
complex, realistic blade geometries. By employing the iVABS design framework,
we have been able to evaluate large numbers of candidate designs efficiently,
narrowing down to configurations that meet demanding structural targets such as
stiffnesses, strength constraints, and weight requirements. This level of
accuracy and computational speed would be extremely challenging to achieve with
traditional 3D finite element modeling alone.
In the current phase of the project, VABS/iVABS is being used to incorporate manufacturing constraints directly into the design process, enabling more realistic geometry parameterization, said Song. The blade template includes features such as rounded spar corners, airfoil trailing-edge treatment, continuous skin laminates, and variable spar thickness along the span. These details not only improve structural fidelity in the analysis but also make the designs more directly transferrable into manufacturable hardware.
Integrated Design-Manufacture-Test Campaign of Composite Rotor Blade
Coupling the iVABS design framework, manufacturing processes, and experimental procedures is essential for achieving realistic blade designs that perform as predicted, said Brett Dalrymple, graduate student in the PSU VLRCOE and recipient of the SMART Fellowship. Prior to developing a full-scale blade, the team fabricated a composite spar using aerospace-grade carbon fiber prepreg materials assembled from an iVABS-derived stacking sequence to validate the manufacturing methodology. After fabrication, the spar was tested to determine cross-sectional and spanwise properties while establishing confidence in the iVABS optimizer by comparing the experimental and analytical results.
Future work will expand this effort by modeling, fabricating, and validating progressively higher-complexity spar configurations, building towards a representative blade section with elements such as an outer composite skin and sandwich core section aft of the spar, said Michael Sheppard, graduate student in the PSU Applied Research Lab. At each phase, experimental measurements will be used to verify and refine the computational results to achieve the desired product. The iVABS framework has also been instrumental in predicting failure loads prior to physical testing, enabling informed experimental planning while strengthening the correlation between analysis and testing.
The VABS program is a uniquely powerful tool for modeling composite blades, high aspect ratio wings, and other slender structures, commonly called beams, said Dr. Wenbin Yu, CTO of AnalySwift. VABS reduces analysis time from hours to seconds by quickly and easily achieving the accuracy of detailed 3D finite element analysis (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 center 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.
Published: 14 Apr 2026
Penn State Vertical Lift Research Center of Excellence is
pushing the boundaries of composite rotorcraft blade development by advancing
the iVABS framework toward a true design-to-production workflow. The initiative
focuses on embedding manufacturing constraints directly into the early-stage
design process, an area historically overlooked in simulation-driven composite
development.
Penn State has been participating in its
Academic Partner Program (APP), and have been using AnalySwift s VABS
simulation software as well as the open source iVABS tool to improve the
manufacturability of composite rotor blades used for helicopters, air mobility,
and other rotorcraft.
AnalySwift, LLC., is a provider of efficient high-fidelity
modeling software for composites. The work is part of the Penn State
Vertical Lift Research Center of Excellence (VLRCOE), a premier research and
education hub at Penn State dedicated to advancing vertical lift technologies, such
as helicopters, drones, and VTOL systems, in key areas like aeromechanics,
flight dynamics, propulsion, acoustics, and survivability.
The APP offers participating universities no-cost licenses
of engineering software programs VABS and SwiftComp so students, researchers,
and faculty can leverage the tools in their academic research.
The VABS program is a general-purpose
cross-sectional analysis tool for predicting structural beam properties and
recovering 3D stresses, strains, and strengths of slender composite
structures. It is a powerful tool for modeling composite rotorcraft
(helicopter, air mobility, unmanned aerial vehicles) and wind turbine rotor
blades, as well as other slender composite structures, such as propellers,
landing gear, and high-aspect ratio wings.
iVABS is a VABS-based structural design
framework, enables VABS for design and optimization, parametric
studies, and uncertainty quantifications in a user-friendly way. This framework
bundles PreVABS, VABS, GEBT, and third-party tool Dakota, along with Python for
integration among these codes and other codes.
We are excited by the work being done by the VLRCOE at Penn State and pleased they have found VABS helpful as they further advance the iVABS platform, said Allan Wood, president & CEO of AnalySwift. As a versatile cross sectional analysis tool, VABS delivers high-fidelity results early on to help computationally resolve engineering challenges, reduce trial and errors, and arrive at the best solution more quickly.
Full-Scale Composite Rotor Blade Optimization with Manufacture
Awareness
The optimization of rotor blade design plays a critical
role in improving overall rotorcraft performance, said Jiwoo Song, who is pursuing a PhD degree in aerospace engineering at Penn State. Recent
advancements in computational toolchains, such as iVABS, enable rapid
exploration of design spaces while satisfying prescribed performance
objectives. The goal of the project is to achieve a design-to-production capability
by developing a drastically more manufacturing-aware iVABS blade design
framework. Looking ahead, this project aims to move beyond virtual optimization
into physical realization, with plans to fabricate a composite rotor blade in
collaboration with the Penn State Applied Research Laboratory, validating the
computational design process through experimental testing.
The VABS software has been central to my research in rotor
blade structural optimization,
continued Song. Its high-fidelity cross-sectional analysis capability
allows me to rapidly compute stiffness, mass, and coupling properties for
complex, realistic blade geometries. By employing the iVABS design framework,
we have been able to evaluate large numbers of candidate designs efficiently,
narrowing down to configurations that meet demanding structural targets such as
stiffnesses, strength constraints, and weight requirements. This level of
accuracy and computational speed would be extremely challenging to achieve with
traditional 3D finite element modeling alone.
In the current phase of the project, VABS/iVABS is being used to incorporate manufacturing constraints directly into the design process, enabling more realistic geometry parameterization, said Song. The blade template includes features such as rounded spar corners, airfoil trailing-edge treatment, continuous skin laminates, and variable spar thickness along the span. These details not only improve structural fidelity in the analysis but also make the designs more directly transferrable into manufacturable hardware.
Integrated Design-Manufacture-Test Campaign of Composite Rotor Blade
Coupling the iVABS design framework, manufacturing processes, and experimental procedures is essential for achieving realistic blade designs that perform as predicted, said Brett Dalrymple, graduate student in the PSU VLRCOE and recipient of the SMART Fellowship. Prior to developing a full-scale blade, the team fabricated a composite spar using aerospace-grade carbon fiber prepreg materials assembled from an iVABS-derived stacking sequence to validate the manufacturing methodology. After fabrication, the spar was tested to determine cross-sectional and spanwise properties while establishing confidence in the iVABS optimizer by comparing the experimental and analytical results.
Future work will expand this effort by modeling, fabricating, and validating progressively higher-complexity spar configurations, building towards a representative blade section with elements such as an outer composite skin and sandwich core section aft of the spar, said Michael Sheppard, graduate student in the PSU Applied Research Lab. At each phase, experimental measurements will be used to verify and refine the computational results to achieve the desired product. The iVABS framework has also been instrumental in predicting failure loads prior to physical testing, enabling informed experimental planning while strengthening the correlation between analysis and testing.
The VABS program is a uniquely powerful tool for modeling composite blades, high aspect ratio wings, and other slender structures, commonly called beams, said Dr. Wenbin Yu, CTO of AnalySwift. VABS reduces analysis time from hours to seconds by quickly and easily achieving the accuracy of detailed 3D finite element analysis (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 center 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.
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