ACCOMPLISHMENTS Developed software to predict turbomachinery flutter. The

software was developed into 2-D and 3-D versions

Adopted software to analyze unsteady transport of vapor/liquid mixtures into complex internal flow geometries

Developed aeroelastic and structural modeling technologies for dynamic modeling of helicopter rotor systems

COMMERCIALIZATION

Received $475,500 from New Jersey pharmaceutical companies for adapting the software for inhaler design to deliver medication

Used the 3-D flow code in consulting with Washington Public Power Supply System. Received $96K

The aeroelastic and structural modeling codes have generated $113K in licensing and $270K in contract research support. An additional 56K is expected

Continuum Dynamics, IncEwing, NJ

SmallBusinessInnovation Research

GOVERNMENT/SCIENCE APPLICATIONS

Code has application to rotorcraft design and has submarine application

Applicable to sonic boom penetration studies in coastal waters for environmental impact on marine life

Useful to higher order compact algorithm for studying acoustic problems

Glenn Research CenterMaterials3-071

Computational Method for Aeroelastic Problem in Turbomachinery

INNOVATION

1988 & 1993 Phase II, NAS3-98024 &NAS3-27631, 6/01NASA Contact – John M. LuceroCompany Contact – Alan Billanin

A state-of-the-art nonlinear codefor cascades and rotors