Nonintrusive Diagnostics for Off-Body Measurements in Flight Experiments

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$100,000.00
Award Year:
2011
Program:
STTR
Phase:
Phase I
Contract:
FA9550-11-C-0091
Award Id:
n/a
Agency Tracking Number:
F10B-T07-0169
Solicitation Year:
2010
Solicitation Topic Code:
AF10-BT07
Solicitation Number:
2010.B
Small Business Information
PO Box 6971, Chesterfield, MO, -
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
126752018
Principal Investigator:
MarkRennie
Research Assistant Prof.
(574) 631-1695
rrennie@nd.edu
Business Contact:
AlanCain
President
(314) 373-3311
abcain@itacllc.com
Research Institute:
University of Notre Dame
Mike Zenk
104 Hessert Laboratory
Notre Dame, IN, 46556-5684
(574) 631-3755

Abstract
ABSTRACT: Flight tests of hypersonic maneuvering vehicles are a challenging but necessary endeavor. While ground tests and numerical simulations can provide important guidance regarding vehicle performance, they are both limited in their reach. Likewise surface-based measurements during flight tests provide valuable information, but do not provide sufficient insight into the complex flowfield to allow unambiguous conclusions to be drawn from the flight data. To address the need for off-body measurements in flight experiments, the University of Notre Dame and ITAC, LLC are partnering to investigate the possibility of using laser-based aero-optic techniques. The proposed Phase I STTR will demonstrate the essential components of the approach in a supersonic ground test facility. The technology developed in this project offers the possibility of in-flight off-body flowfield measurements for a variety of purposes, including hypersonic weapon system flight tests and, potentially, as part of a high speed store separation control system. BENEFIT: By providing a clearer picture of the flowfield around a flight test vehicle, the proposed technology will allow deeper insight into the phenomena experienced by the vehicle. In this manner, many issues which must remain ambiguous when testing with current technology could be definitely determined. This will allow the development of safer and more reliable systems, which will consistently perform in a predictable manner because the flight envelope will be better understood.

* information listed above is at the time of submission.

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