SBIR/STTR Research Award

3D Flow Field Measurements using Aerosol Correlation Velocimetry

Award identifier c1990fcaed9048ad97915341619bccba2483303809d06ade8d6756941e3d90feAwarding agency National Aeronautics and Space Administration

Award amount

$749,998

Program and phase

SBIR · Phase II

Award year

2016

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
AeroMancer Technologies Corporation
Proposal award date
2016-09-29
Contract end date
2018-09-28
UEI
VSMKX9PLQMQ9
Solicitation number
Not reported
Topic code
A1.08

Research abstract

AeroMancer Technologies proposes to develop a 3D Global Lidar Airspeed Sensor (3D-LGAS) using Aerosol Correlation Velocimetry for standoff sensing of high-resolution spatially and temporally resolved three-component global airspeeds using a scanning elastic lidar. The proposed instrument uses range-resolved elastic backscatter data from a scanning lidar beam to generate a 3D map of aerosol density in a short time span. Aerosol density fluctuations are cross-correlated between successive scans to obtain the displacements of the aerosol features along the three axes. Current methods of non-intrusive global airspeed measurement include Particle Imaging Velocimetry (PIV) and Doppler Global Velocimetry (DGV). Common drawbacks of these methods are that they require precise alignment of separate transmitters and receivers; and it is expensive and unwieldy to extend these measurements for use in medium and large wind tunnels. In Phase I, AeroMancer identified the main requirements of the application and the instrument; developed a conceptual design of a Phase II prototype; identified 3D airspeed extraction algorithms; and benchmarked the performance of the prototype using experiments and numerical simulations. In Phase II, AeroMancer will develop the final design of the prototype by finalizing the requirements; and by performing trade studies and an eye safety analysis to select major components. The prototype will then be fabricated, assembled and packaged for wind tunnel use. Algorithms for the extraction of 3D global airspeeds, turbulence and solid object identification will be developed. Different scanning approaches will be developed and sources of error in the measurement will be analyzed and quantified. Software packages for control, data acquisition, storage and processing will be developed. The prototype will be tested in the laboratory for alignment, calibration, verification and validation. Limited wind tunnel testing will be performed if resources permit.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

6 SBIR/STTR records share this UEI (2015–2020). Reported award amounts total $2,261,386. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration

Agency intelligence

National Aeronautics and Space Administration

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