High Frequency Surface Pressure, Shear Stress and Heat Flux Measurements for High Temperature Applications

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$99,071.00
Award Year:
2007
Program:
STTR
Phase:
Phase I
Contract:
FA9550-07-C-0129
Award Id:
83334
Agency Tracking Number:
F074-014-0270
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
840 University City Blvd, Suite 4, Blacksburg, VA, 24060
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
133461553
Principal Investigator:
JonGreene
Chief Technology Officer
(540) 953-1796
jgreene@lambdainc.com
Business Contact:
JonGreene
Chief Technology Officer
(540) 953-1796
jgreene@lambdainc.com
Research Institute:
VIRGINIA TECH
Walter O'Brien
Dept. of Mech. Engineering
109 Randolph Hall
Blacksburg, VA, 24061
(540) 231-9104
Nonprofit college or university
Abstract
Lambda Instruments, Inc., in cooperation with Virginia Tech and Pratt & Whitney, propose to investigate the feasibility of developing ultra high-temperature, high-frequency sapphire optical fiber-based sensors for next generation hypersonic vehicle sensors and wind tunnel testing programs up to 3600 degreesF. The capability to accurately measure the surface pressure, skin friction, and temperature gradient imposed on a body subjected to high speed flow is a vital first step toward improving the performance of future hypersonic vehicles. Although real-time determination of these parameters has been an on-going challenge since the early days of flight, only in the last 15 years has attention shifted to hypersonic conditions due to sensor advancements in miniaturization, sensitivity, and mounting techniques. Accurate measurements of aerodynamic heating is a major concern at hypersonic speeds. Temperature sensors used to monitor the thermal profile can also give insight into determining the peak in a shock interaction region or the boundary layer transition. Finally, current air-breathing hypersonic vehicles integrate airframe and engine. The entire fore body of a scramjet vehicle's underside, for example, may be used as an external inlet to provide flow at the perfect condition to the engine. Failure to accurately know or predict surface conditions can lead to engine failure or catastrophic vehicle structural failure.

* information listed above is at the time of submission.

Agency Micro-sites


SBA logo

Department of Agriculture logo

Department of Commerce logo

Department of Defense logo

Department of Education logo

Department of Energy logo

Department of Health and Human Services logo

Department of Homeland Security logo

Department of Transportation logo

Enviromental Protection Agency logo

National Aeronautics and Space Administration logo

National Science Foundation logo
US Flag An Official Website of the United States Government