Transistion Control in Corner Flow of a Supersonic Square Nozzle

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$67,548.00
Award Year:
1994
Program:
SBIR
Phase:
Phase I
Contract:
n/a
Agency Tracking Number:
22538
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
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
n/a
Principal Investigator:
Ray-Sing Lin
(804) 865-0818
Business Contact:
() -
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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