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Company Information:

Company Name: ENGINEERING RESEARCH & ANALYSIS CO.
City: DAYTON
State: OH
Zip+4: -
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
Website URL: N/A
Phone: (937) 291-3800

Award Totals:

Program/Phase Award Amount ($) Number of Awards
SBIR Phase I $689,679.00 8
SBIR Phase II $3,303,491.00 5

Award List:

An Innovative Variable Geometry Advanced Dual-Lip Airblast Fuel Nozzle

Award Year / Program / Phase: 1995 / SBIR / Phase I
Agency: NASA
Principal Investigator: Mohammed A. Mawid , President
Award Amount: $70,000.00

High Fuel-Air Ratio (FAR) Combustor Modeling

Award Year / Program / Phase: 2002 / SBIR / Phase I
Agency / Branch: DOD / NAVY
Principal Investigator: Mohammed A. Mawid, Technical Director
Award Amount: $69,999.00
Abstract:
"A high fuel-air ratio combustor/turbine computational model (computer code) is proposed for development in this SBIR project. The proposed computational model will address fuel-air ratio and temperature non-uniformities and fluctuations at the combustorand 1st stage high pressure turbine exit… More

High Fuel-Air Ratio (FAR) Combustor Modeling

Award Year / Program / Phase: 2003 / SBIR / Phase II
Agency / Branch: DOD / NAVY
Principal Investigator: Mohammed Mawid, President & Technical Dir
Award Amount: $749,684.00
Abstract:
A high fuel-air ratio combustor computational model (computer code) is proposed for development in this SBIR project. The proposed computational model will address fuel-air ratio and temperature non-uniformities and fluctuations at the combustor and 1ststage high pressure turbine exit planes based… More

Control of Fuel Atomization and Mixing for Emission Reduction in High Performance Gas Turbines

Award Year / Program / Phase: 2004 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Mohammed A. Mawid, Technical Director
Award Amount: $99,808.00
Abstract:
An innovative ariblast-based single-lip fuel injector with piloted fuel for advanced military gas turbine combustors is proposed for development in this SBIR. The proposed innovative fuel injector design concept will significantly improve the mixing performance of fuel and air in the vicinity of the… More

Control of Fuel Atomization and Mixing for Emission Reduction in High Performance Gas Turbines

Award Year / Program / Phase: 2005 / SBIR / Phase II
Agency / Branch: DOD / USAF
Principal Investigator: Mohammed A. Mawid, Technical Director
Award Amount: $749,981.00
Abstract:
An innovative piloted airblast fuel injector concept called "SAWBLAST" is proposed for development. Phase-I work demonstrated the potential of the proposed SAWBLAST concept through detailed CFD analyses for improved performance over existing piloted aiblast fuel injectors. Phase-II efforts will… More

Pulse Detonation Engines Cycle Analysis and Performance Prediction Code

Award Year / Program / Phase: 2007 / SBIR / Phase I
Agency / Branch: DOD / NAVY
Principal Investigator: Mohammed A. Mawid, Technical Leader
Award Amount: $69,981.00
Abstract:
A transient performance PDE code is proposed for development and demonstration in this SBIR project. The proposed formulation methodology for the performance code is based upon a zero-order time-marching methodology to compute PDE properties as a function of PDE cycle time. The proposed PDE code… More

Improved Heat Release Model for Augmentor Screech Characterization

Award Year / Program / Phase: 2007 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Mohammed A. Mawid, Technical leader
Award Amount: $99,951.00
Abstract:
A new unique reduced order heat release model is proposed for development in this SBIR. The proposed reduced order heat release model is derived based on the prevailing local flow conditions and it expresses the complex relationship between the fluctuating heat release and the fluctuating local… More

Improved Damping Modeling for Afterburners

Award Year / Program / Phase: 2008 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Mohammed Mawid, Technical Director
Award Amount: $99,949.00
Abstract:
A novel damping model to damp acosutic pressures in gas turbine afterburners is proposed for development and validation in this SBIR project. The proposed model will account for as many of the physical phenomena present in the afterburenr as possible which will include grazing, bias, and mean flows,… More

Pulse Detonation Engines Cycle Analysis and Performance Prediction Code

Award Year / Program / Phase: 2008 / SBIR / Phase II
Agency / Branch: DOD / NAVY
Principal Investigator: Mohammed A. Mawid, Senior Scientist
Award Amount: $303,927.00
Abstract:
An integrated Pulse Detonation Engine (PDE)and Airframe Transient Cycle Analysis and Airframe Performance (PDE-CAASP) code is proposed for development based upon the successful development of a PDE Transient Cycle Analysis Code during Phase-I. The Integrated PDE/Airframe code will include flight… More

Passive Mixing Enhancers for Improved Flame Spreading and Propagation

Award Year / Program / Phase: 2009 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Mohammed A. Mawid, Sr. Scientist
Award Amount: $99,991.00
Abstract:
A new inovative passive mxing enhancer design concept is proposed for development and implementation in either turbine engine augmentor and/or main combustor. The design concept utilzes certain geometrical features to create and induce significant amounts of axial vorticity that leads to enhanced… More

Improved Damping Modeling for Afterburners

Award Year / Program / Phase: 2009 / SBIR / Phase II
Agency / Branch: DOD / USAF
Principal Investigator: Mohammed A. Mawid, technical Director
Award Amount: $749,905.00
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… More

Passive Mixing Enhancers for Improved Flame Spreading and Propagation

Award Year / Program / Phase: 2011 / SBIR / Phase II
Agency: DOD
Principal Investigator: Mohammed A. Mawid, Senior Scientist – (937) 291-3800
Award Amount: $749,994.00
Abstract:
A novel multi-lobe flame holder design concept was designed, fabricated, and tested under high vitiated air flow temperature conditions for Light-Off (LO)and Lean Blow Out (LBO) performance. The new novel flame holder concept clearly demonstrated an improved LO/LBO performance pver the conventional… More

Technologies for the Suppression of Combustion Instability or Screech

Award Year / Program / Phase: 2013 / SBIR / Phase I
Agency: DOD
Principal Investigator: Mohammed Mawid, Technical Director – (937) 291-3800
Award Amount: $80,000.00
Abstract:
A novel passive screech liner damping design concept to damp out low and high order screech modes simultaneously in legacy, pipeline, and advanced military afterburners are proposed for development and demonstration in this SBIR project. The proposed novel passive damping liner design concept is… More