NASA SBIR SUCCESS STORY 

 ARCHIVED - Data Not Current
 For Information Purposes Only

Glenn Research Center  
1989 Phase II 

Flow in Turbine Blade Passages 

Scientific Research Associates, Inc. 

Glastonbury, CT 
 

INNOVATION 
The use of refractive index matching laser velocimetry to obtain detailed mean and turbulent flow fields
Laser-Doppler Velocimeter Set-up-Forward Scattering
Laser-Doppler Velocimeter 
Set-up-Forward Scattering
ACCOMPLISHMENTS 
  • Obtained knowledge of flow fields required to achieve goals
  • Flow field measurements provided a nice compliment to previously acquired heat transfer from a model of similar geometry
  • Simulations were compared to experimental velocity fields
  • Combined computational-experimental program provided new insight into structure of flow field
COMMERCIALIZATION 
  • Generated $240K in Government Non SBIR/STTR Funds
  • UTRC collaborated in the program by providing model geometry and heat transfer data
  • Pratt and Whitney performed the computational calculations
GOVERNMENT/SCIENCE APPLICATIONS 
  • New design tool for the development of turbine blade internal cooling configurations
  • Rotating flow field database useful for simulation code validation
For more information about this firm, please send e-mail to company representative 

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Curator: SBIR Support                   3/17/06