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Aero Systems Engineering, Inc.
UEI: M6SWVFKC1997
# of Employees: 180
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
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Gas Turbine Engine Exhaust Jet Shear-layer Pressure Measurement System
Amount: $999,742.00A microphone array system for studying the near field hydrodynamic region adjacent to the supersonic exhaust plume of a tactical aircraft engine in a ground test fixture at approximately 20 feet above ...
SBIRPhase II2013Department of Defense Navy -
Alternatives to Gold-Plate Engines for Test Cell Correlation
Amount: $149,853.00ABSTRACT: The traditional approach to establishing test cell correlation factors is expensive and time consuming requiring multiple engine runs to establish a parametric database for comparison. Whil ...
SBIRPhase I2012Department of Defense Air Force -
Gas Turbine Engine Exhaust Jet Shear-layer Pressure Measurement System
Amount: $79,984.00A microphone array system for studying the near field hydrodynamic region adjacent to the supersonic exhaust plume of a tactical aircraft engine in a ground test fixture at approximately 20 feet above ...
SBIRPhase I2011Department of Defense Navy -
Fan Noise Screening Rig for New Open Rotor and Propeller Concepts
Amount: $99,760.00Recent advancements in open rotor engine concepts warrant continued research, however the cost of wind tunnel tests is not insignificant. Because the jet noise of an open rotor engine, or even that o ...
SBIRPhase I2010National Aeronautics and Space Administration -
Practical Assessment of Noise/Performance Trade for High NPR Nozzles
Amount: $999,145.00With improvements in high performance military jet aircraft engines and the increase in complexity of the exhaust systems the noise produced has become problematic. Reducing these noise levels, while ...
SBIRPhase II2009Department of Defense Navy -
Practical Assessment of Noise/Performance Trade for High NPR Nozzles
Amount: $137,355.00With improvements in high performance military jet aircraft engines and the increase in complexity of the exhaust systems the noise produced has become problematic. Reducing these noise levels, while ...
SBIRPhase I2007Department of Defense Navy -
Flow-Field Seeding Techniques for Large Transonic Wind Tunnels
Amount: $99,489.00Optical measurements including laser velocimetry (LV), particle image velocimetry (PIV), and other similar techniques are becoming a more important part of aerodynamic testing. However their implement ...
SBIRPhase I2006Department of Defense Air Force -
Acoustic Test Method for Turbofan Engine Exhaust Systems at Cruise Conditions
Amount: $572,250.00The exhaust flow from a turbofan engine operating at typical cruise conditions generates noise as turbulent flow interacts with the basic shock cell pattern. This can be a significant source of noise ...
SBIRPhase II2004National Aeronautics and Space Administration -
Acoustic Test Method for Turbofan Engine Exhaust Systems at Cruise Conditions
Amount: $67,606.00The exhaust flow from a turbofan engine operating at typical cruise conditions generates noise as turbulent flow interacts with the basic shock cell pattern. This can be a significant source of noise ...
SBIRPhase I2003National Aeronautics and Space Administration -
New Method for Determination of Acoustic Signatures in Wind Tunnel Testing
Amount: $99,936.00"The acoustic signature generated by test articles in high speed wind tunnel tests is difficult to measure due to the high level of background noise created by the wind tunnel flow. A unique research ...
SBIRPhase I2002Department of Defense Air Force
