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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
Contract: N/A
Agency Tracking Number: 22538
Amount: $67,548.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: N/A
Solicitation Number: N/A
Timeline
Solicitation Year: N/A
Award Year: 1994
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
28 Research Drive
Hampton, VA 23666
United States
DUNS: N/A
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
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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