Publikationsdatum:
2019-07-12
Beschreibung:
COREL and W12SC3 useful in aerodynamic design and analysis of wings for supersonic speeds. COREL (Conical Relaxation) program solves nonlinear full potential equation for spanwise section of wing in crossflow plane, and option exists to correct result for nonconical geometry. W12SC3 applies lineartheory panel methods to compute solutions for wing/body configuration. Programs restricted to supersonic flows and useful for many design, analysis, and optimization applications. COREL and W12SC3 written in FORTRAN IV for batch execution.
Schlagwort(e):
MACHINERY
Materialart:
LAR-13239
,
NASA Tech Briefs (ISSN 0145-319X); 10; 2; P. 106
Format:
text
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