Aero Systems Engineering, Inc.

Basic Information

358 East Fillmore Avenue
St. Paul, MN, -

http://www.aseholdings.com

Company Profile

n/a

Additional Details

Field Value
DUNS: 41776824
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 180


  1. Gas Turbine Engine Exhaust Jet Shear-layer Pressure Measurement System

    Amount: $999,742.00

    A 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 ...

    SBIR Phase II 2013 Department of Defense Navy
  2. Alternatives to Gold-Plate Engines for Test Cell Correlation

    Amount: $149,853.00

    ABSTRACT: 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 ...

    SBIR Phase I 2012 Department of Defense Air Force
  3. Gas Turbine Engine Exhaust Jet Shear-layer Pressure Measurement System

    Amount: $79,984.00

    A 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 ...

    SBIR Phase I 2011 Department of Defense Navy
  4. Fan Noise Screening Rig for New Open Rotor and Propeller Concepts

    Amount: $99,760.00

    Recent 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 ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  5. Practical Assessment of Noise/Performance Trade for High NPR Nozzles

    Amount: $999,145.00

    With 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 ...

    SBIR Phase II 2009 Navy Department of Defense
  6. Practical Assessment of Noise/Performance Trade for High NPR Nozzles

    Amount: $137,355.00

    With 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 ...

    SBIR Phase I 2007 Navy Department of Defense
  7. Flow-Field Seeding Techniques for Large Transonic Wind Tunnels

    Amount: $99,489.00

    Optical 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 ...

    SBIR Phase I 2006 Air Force Department of Defense
  8. Acoustic Test Method for Turbofan Engine Exhaust Systems at Cruise Conditions

    Amount: $572,250.00

    The 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 ...

    SBIR Phase II 2004 National Aeronautics and Space Administration
  9. Acoustic Test Method for Turbofan Engine Exhaust Systems at Cruise Conditions

    Amount: $67,606.00

    The 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 ...

    SBIR Phase I 2003 National Aeronautics and Space Administration
  10. 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 ...

    SBIR Phase I 2002 Air Force Department of Defense

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