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Transistion Control in Corner Flow of a Supersonic Square Nozzle

Award Information

Agency:
National Aeronautics and Space Administration
Branch:
N/A
Award ID:
22538
Program Year/Program:
1994 / SBIR
Agency Tracking Number:
22538
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
High Technology Corporation
28 Research Drive Hampton, VA 23666
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Woman-Owned: No
Minority-Owned: Yes
HUBZone-Owned: No
 
Phase 1
Fiscal Year: 1994
Title: Transistion Control in Corner Flow of a Supersonic Square Nozzle
Agency: NASA
Contract: N/A
Award Amount: $67,548.00
 

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

Principal Investigator:

Ray-Sing Lin
8048650818

Business Contact:

Small Business Information at Submission:

High Technology Corp.
28 Research Drive Hampton, VA 23666

EIN/Tax ID:
DUNS: N/A
Number of Employees: N/A
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No