NASA SBIR 2020-I Solicitation

Proposal Summary


PROPOSAL NUMBER:
 20-1- A1.08-4810
SUBTOPIC TITLE:
 Aeronautics Ground Test and Measurement Technologies
PROPOSAL TITLE:
 Global Skin Friction Sensor for Cryogenic Wind Tunnels
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Innovative Scientific Solutions, Inc.
7610 McEwen Road
Dayton, OH 45459
(937) 429-4980

Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)

Name:
Jim Crafton
E-mail:
jwcrafton@innssi.com
Address:
7610 McEwen Road Dayton, OH 45459 - 3908
Phone:
(937) 630-3012

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)

Name:
Larry Goss
E-mail:
gosslp@innssi.com
Address:
7610 McEwen Road Dayton, OH 45459 - 3908
Phone:
(937) 429-4980
Estimated Technology Readiness Level (TRL) :
Begin: 5
End: 6
Technical Abstract (Limit 2000 characters, approximately 200 words)

While skin friction is a key parameter for characterizing fluid flows, it has proven to be a difficult quantity to measure. Currently, skin friction is measured at discrete locations using different sensors; however, determining the proper measurement locations a priori is a significant challenge. Measurement techniques that provide global distributions of skin friction, such as oil film interferometry, shear sensitive liquid crystals, and surface stress sensitive films, have demonstrated steady state skin friction distributions in specific settings. Unfortunately, deployment of these measurement techniques into cryogenic wind tunnels has proven difficult. A system that can provide global measurements of mean and unsteady skin friction is of significant interest. ISSI and WMU propose exploiting existing measurement systems for temperature and utilizing a new variational mathematical approach that can extract global skin friction from high spatial resolution distributions of surface temperature acquired using Temperature-Sensitive Paint (TSP) and IR thermography. The process is based on the well-established relationship between the energy equation and skin friction. This approach has recently been demonstrated by the proposing team as part of a Phase II Air Force SBIR program, thus demonstrating the technical maturity of the technique. Temperature-Sensitive Paint and IR thermography are high TRL tools that are currently used in wind tunnels at both room temperature and cryogenic conditions. These systems, combined with surface heating devices such as carbon nanotubes, provide the high spatial resolution measurements of temperature gradients that are required for extraction of skin friction using this new approach. Combining the proven measurement capabilities of TSP and IR thermography with this new variational approach to extraction of skin friction results in a low risk approach to providing global skin friction measurements in cryogenic wind tunnels.

Potential NASA Applications (Limit 1500 characters, approximately 150 words)

The SFW program has developed a model to assess the capabilities of various computational techniques, FAITH Hill. Fluctuating aerodynamic loads are a significant concern for the SLS program as unsteady aerodynamic pressures can excite the vehicle dynamic modes. Experimental measurements from the proposed sensor would provide each of these programs with heat transfer and flow separation/attachment data to validate computational models. Similar testing capability could be demonstrated in other NASA tunnels as part of a Phase II program.

Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words)

The final product from this program should be a system capable of acquiring high spatial resolution distributions of both heat transfer and skin friction on a model in a cryogenic wind tunnel. This is a technological capability that is of interest to ISSI’s current commercial, research, and military wind tunnel customers. ISSI expects to aggressively market this capability to these customers.

Duration: 6

Form Generated on 06/29/2020 21:01:10