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SOLUTIONS INCREASING THE CONVERGENCE RATE FOR EULER EQUATION

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: N/A
Agency Tracking Number: 581
Amount: $343,614.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: N/A
Solicitation Number: N/A
Timeline
Solicitation Year: N/A
Award Year: 1984
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
510 Clyde Ave.
Mountain View, CA 94043
United States
DUNS: N/A
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 David Nixon
 () -
Business Contact
Phone: () -
Research Institution
N/A
Abstract

EXISTING METHODS OF NUMERICALLY SOLVING THE EULER EQUATIONS EXISTING METHODS OF NUMERICALLY SOLVING THE EULER EQUATIONS USE A LINEARIZATION IN EITHER REAL OR ARTIFICIAL TIME SO THAT AT EACH STEP OF THE SOLUTION PATH WELL KNOWN TECHNIQUESCAN BE USED. THIS LINEARIZATION IS PERFORMED ABOUT THE SOLUTION OBTAINED AT THE PREVIOUS STEP AND SUCH A SOLUTION SATISFIES THE PHYSICAL BOUNDARY CONDITIONS. SPECIAL TREATMENT MAY BE EQUIRED NEAR SHOCK WAVES. AN ALTERNATIVE, NOVEL CONCEPT IS THAT THE LINEARIZATION SHOULD BE PERFORMED ABOUT SOME FUNCTION SET THAT SPEEDS CONVERGENCE, DOES NOT REQUIE SPECIAL TREATMENT OF THE SHOCK AND IS NOT NECESSARILY RELATED TO THE PHYSICAL SOLUTION. THIS PHASE I EFFORT CONCERNS A PROGRAM TO ESTABLISH SOME GUIDELINES ABOUT THE CHOICE OF THIS FUNCTION SET SO THAT OPTIMUM USE CAN BE MADE OF THE GENERAL CONCEPT.

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

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