 |
Glenn
Research Center
1988 & 1993
Phase 2 Computational
Method for Aeroelastic Problems in Turbomachinery
Continuum
Dynamics, Inc.
Ewing, NJ |
INNOVATION
A state-of-the-art
nonlinear aeroelastic code for cascades and rotors |
3D Aeroelastic Response for Rotor-Stator
|
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 $475K 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 and received $96K
- The aeroelastic and structural
modeling codes have generated $113K in licensing and $270K in contract
research support. An additional $56K is expected
|
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
|
| For more
information about this firm, please send e-mail to company
representative Return
to NASA SBIR Success Listings |
Power/Propulsion
Curator:
SBIR Support 4/25/05 |
