Nonlinear Data Analysis Tool for Scramjets and Other Engines

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$124,861.00
Award Year:
2012
Program:
SBIR
Phase:
Phase I
Contract:
NNX12CF17P
Award Id:
n/a
Agency Tracking Number:
114573
Solicitation Year:
2011
Solicitation Topic Code:
A2.02
Solicitation Number:
n/a
Small Business Information
TN, Tullahoma, TN, 37388-5583
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
144158677
Principal Investigator:
Eric Jacob
Principal Investigator
(931) 455-7333
eric.jacob@gtlcompany.com
Business Contact:
Paul Gloyer
Business Official
(931) 581-6134
paul.gloyer@gtlcompany.com
Research Institution:
Stub




Abstract
The UCDS process is the result of 50 years of research into combustion instability by the worlds leading scientists and engineers. The breakthroughs that created UCDS have provided a solid analytical foundation upon which tools can be developed and applied. One of these is the UCDS nonlinear tool, which GTL has been applying with much success in the investigations of the dynamics of solid rockets, liquid rockets and turbojets. In the proposed effort, GTL shall enhance this tool in preparation for its application to scramjets and ramjets by incorporating mean flow effects in the acoustic models used in the nonlinear algorithms. Since the Nonlinear Data Analysis Tool (NDAT) shares the same nonlinear algorithm with the UCDS nonlinear tool, this enhancement shall also improve the ability of NDAT to transform nonlinear test data into linear parameters. Taking this to the next step, GTL shall increase the functionality of NDAT by implementing changes to the algorithm that allow it to utilize the data from multiple pressure transducers in the data analysis rather than restricting the tool to the current single data channel. This will be accomplished by developing algorithm routines that use the relative location of the pressure transducers and the intervening acoustic environment to account for the temporal and phase relationships between the data streams. When implemented, these changes will allow NDAT to automatically identify the orientation of the oscillating modes and reduce the nonlinear pressure oscillation data into a clear and concise set of linear parameters. The last part of the Phase I effort will be to examine the role of nonlinear energy dissipation in scramjets in preparation for further refinement in the Phase II effort.

* information listed above is at the time of submission.

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