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Universal PDV System for Wind Tunnel Tests

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: F40600-02-C-0016
Agency Tracking Number: 021XP-1276
Amount: $99,964.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: N/A
Solicitation Number: N/A
Timeline
Solicitation Year: N/A
Award Year: 2002
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
2572 White Road
Irvine, CA 92614
United States
DUNS: 188465819
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Robert McKenzie
 Senior Scientist
 (408) 732-4858
 rmckenzie@metrolaserinc.com
Business Contact
 Cecil Hess
Title: President
Phone: (949) 553-0688
Email: chess@metrolaserinc.com
Research Institution
N/A
Abstract

"We propose a versatile and affordable Planar Doppler Velocimetry (PDV) system for wind tunnel measurements capable of simultaneously measuring velocity, pressure, and temperature everywhere in the field of view. The system expands upon our recentexperience where a PDV system was used to demonstrate the first successful measurements of spatially and temporally resolved, three-dimensional, velocity vector fields in the blade wakes of a full-scale, operating rotor. A PC-based software included withthe PDV system will incorporate advanced and experimentally validated algorithms to fully accommodate the time-dependent aerodynamic flows, and will provide near-autonomous processing procedures and image displays with the minimum requirements for operatorexpertise and training. The tasks described in this proposal are essential steps leading to a universal PDV system that can be routinely applied to wind tunnel aerodynamics testing programs, and subsequently commercialized. The impact of advances in PDVtechnology and its subsequent transfer to future aerodynamic testing programs will be substantial. This expectation is particularly relevant to testing programs for large and full-scale wind tunnel aircraft and missile models because many aspects of flowfield aerodynamics are not thoroughly understood nor adequately predictable, due in part to the lack of detailed measurement capabilities. The availability of advanced PDV instrumentation will a

* Information listed above is at the time of submission. *

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