Improved Damping Modeling for Afterburners

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$749,905.00
Award Year:
2009
Program:
SBIR
Phase:
Phase II
Contract:
FA8650-09-C-2916
Award Id:
86623
Agency Tracking Number:
F073-055-1217
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
ENGINEERING RESEARCH & ANALYSIS COMPAN (Currently ENGINEERING RESEARCH & ANALYSIS CO.)
340 SENTINEL OAK DRIVE, DAYTON, OH, 45458
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
966649048
Principal Investigator:
Mohammed Mawid
technical Director
(937) 291-3800
mohammed.mawid@engineeringrac.com
Business Contact:
Mohammed Mawid
Owner
(937) 291-3800
mohammed.mawid@engineeringrac.com
Research Institution:
n/a
Abstract
A Three-Dimensional Damping (TDD) Model and an Alpha V1.1 computer code successfully developed and demonstrated in Phase-I will be further developed to include additional important processes such as unsteady heat release and sheared flows. In addition, aero-acoustics and screech tests will be conducted to obtain a set data for model validation and evaluation. BENEFIT: The proposed Three-Dimensional Damping (TDD) Model and the computer code will greatly benefit turbine engines OEM to better design screech liners and predict the acoustic modes that will be excited by the unsteady heat release. Such a model currently does not exist and will potentially replace the current lumped parameter-based screech liners design practices. The developed code will be transitioned to a turbine engine OEM that will utilize to improve their screech liners design to damp out both high and low order excited modes.

* information listed above is at the time of submission.

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