Technique analyzes viscosity-dependent aerodynamic characteristics of multielement infinite swept wings in incompressible flow. Use of source distributions rather than displacement thickness to represent boundary layer effect on potential flow and of iterative technique for matrix inversion reduces computer time for overall analysis.
Swept wing aerodynamics
NASA Tech Briefs ; 1 , 3
1977-01-01
Sonstige
Keine Angabe
Englisch
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