SBIR/STTR Research Award
Planar Doppler Velocimetry for Aircraft Exhausts
Award amount
$149,868Program and phase
STTR · Phase IAward year
2011Award details
- Awarding agency
- Department of Defense
- Branch
- Navy
- Recipient company
- METROLASER, INCORPORATED
- Proposal award date
- 2011-08-15
- Contract end date
- Not reported
- UEI
- RB8MDWWD5MF8
- Solicitation number
- 2011.A
- Topic code
- N11A-T004
Research abstract
A diagnostic is proposed for aircraft engine exhausts that provides three velocity components at each point in an image of a slice through the plume. The method measures the Doppler shift of laser light scattered from soot particles naturally present in the exhaust, and may also be useful for measuring non-combustion flows outside the exhaust using naturally occurring environmental aerosols. An image processing filter that employs iodine vapor absorption transforms frequency variations in the scattered light to variations in image intensity. The technique can provide two-dimensional instantaneous velocity profiles over an area large enough to cover the cross-section of a typical aircraft engine exhaust. A laser system that is insensitive to vibration effects makes it suitable for field measurements on a full-scale aircraft. Velocity uncertainties are dependent on signal level, and thus on the level of soot particles present in the flow. However, the method should be capable of operating over a large range of particle loading levels and is capable of measuring supersonic as well as subsonic velocities.
Technology keywords
Not reported
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Three-Component Planar Doppler Velocimetry Measurements in a Full-Scale Aircraft Exhaust
- Planar Doppler Velocimetry for Aircraft Exhausts
- Micro-Plasma Turbulence Velocimetry (uPTV)
- High Resolution Measurement of the Flow Velocity Field in a Supersonic Jet Plume