WE PROPOSE TO WRITE CODES FOR A FAST EVALUATION OF STEADY, COMPRESSIBLE, TWO-DIMENSIONAL, INVISCID FLOWS, EITHER SUBSONIC OR TRANSONIC, WITH OR WITHOUT BOW SHOCKS AND IMBEDDED SHOCKS.

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: N/A
Agency Tracking Number: 2802
Amount: $49,925.00
Phase: Phase I
Program: SBIR
Awards Year: 1985
Solicitation Year: N/A
Solicitation Topic Code: N/A
Solicitation Number: N/A
Small Business Information
Po Box 184, Freeport, NY, 11520
DUNS: N/A
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 DR GINO MORETTI
 PRINCIPAL INVESTIGATOR
 () -
Business Contact
Phone: () -
Research Institution
N/A
Abstract
WE PROPOSE TO WRITE CODES FOR A FAST EVALUATION OF STEADY, COMPRESSIBLE, TWO-DIMENSIONAL, INVISCID FLOWS, EITHER SUBSONIC OR TRANSONIC, WITH OR WITHOUT BOW SHOCKS AND IMBEDDED SHOCKS. THE COMPUTATIONAL SPEED WILL BE PROVIDED BY A NOVEL SWEEPING TECHNIQUE, BASED ON THE "LAMBDA" INTEGRATION SCHEME. THE CONCEPT HAS ALREADY BEEN SUCCESSFULLY APPLIED TO ONE-DIMENSIONAL PROBLEMS. APPLICATIONS WILL BE MADE TO FLOWS IN DUCTS, AIRFOILS AND BLUNT BODIES IN SUPERSONIC FLIGHT.

* Information listed above is at the time of submission. *

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