Publication Date:
2019-06-28
Description:
Integrated system of computer programs, developed for design and analysis of supersonic configurations, uses linearized-theory methods to calculate surface pressures and uses supersonic area-rule concepts in combination with linearized theory to calculate aerodynamic force coefficients. Programs include constraints on linear theory methods to provide physical realism. Package proves useful for any type of supersonic configuration.
Keywords:
MECHANICS
Type:
LAR-12237
,
NASA Tech Briefs (ISSN 0145-319X); 2; 4; P. 3
Format:
text
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