A Novel Computational Tool for Transition Prediction over Hypersonic Vehicles

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$100,000.00
Award Year:
1998
Program:
SBIR
Phase:
Phase I
Contract:
n/a
Agency Tracking Number:
40953
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
HIGH TECHNOLOGY CORP.
28 RESEARCH DRIVE, Hampton, VA, 23666
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
n/a
Principal Investigator:
Mujeeb R. Malik
(757) 865-0818
Business Contact:
() -
Research Institution:
n/a
Abstract
Laminar to turbulent transition phenomenon in hypersonic flows remains poorly understood although it has a profound impact on the thermal protection system weight, vehicle drag and air-breathing engine performance. Transition location uncertainty forces designers to be conservative by adding weight and reducing thrust. Accurate prediction techniques are needed since existing applicable transition databases are insufficient and validated arbitrary configuration prediction codes are non-existent. It is proposed to develop a novel computational tool for hypersonic transition prediction which can account for environmental effects. The computational tool can not only capture the complex physical phenomenon, but also is computationally efficient and, therefore, has the potential of becoming a design tool for aerospace vehicles of the 21st century.

* information listed above is at the time of submission.

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