Computer program developed that provides mathematical solution to design and construction of combustion chambers for jet engines. Improved results in areas of combustor flow fields accomplished by this computerprogram solution, cheaper and quicker than experiments involving real systems for models.
Turbulent Recirculating Flows in Isothermal Combustor Geometries
NASA Tech Briefs ; 8 , 3
1985-01-01
Sonstige
Keine Angabe
Englisch
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