Transistion Control in Corner Flow of a Supersonic Square Nozzle

Award Information
Agency:
National Aeronautics and Space Administration
Amount:
$67,548.00
Program:
SBIR
Contract:
N/A
Solitcitation Year:
N/A
Solicitation Number:
N/A
Branch:
N/A
Award Year:
1994
Phase:
Phase I
Agency Tracking Number:
22538
Solicitation Topic Code:
N/A
Small Business Information
High Technology Corp.
28 Research Drive, Hampton, VA, 23666
Hubzone Owned:
N
Woman Owned:
N
Socially and Economically Disadvantaged:
N
Duns:
N/A
Principal Investigator
 Ray-Sing Lin
 (804) 865-0818
Business Contact
Phone: () -
Research Institution
N/A
Abstract
"Quiet" (low-disturbance) wind tunnels, needed for transitionresearch, require cleverly designed nozzle contours forstabilization or delay of dominant instabilities in supersonicnozzle wall boundary layers. However, if a nozzle of squarecross-section

* information listed above is at the time of submission.

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