Newtonian closed-form expressions for aerodynamic coefficients are developed for complete and partial conic and spheric bodies at combined angles of attack and sideslip; calculations from expressions presented in tabulated form; comparisons of theory with hypersonic experimental data for many shapes.
Tables of aerodynamic coefficients obtained from developed Newtonian expressions for complete and partial conic and spheric bodies at combined angles of attack and sideslip with some comparisons with hypersonic experimental data
NASA -- Tech Report
1962
306 pages
Report
Englisch
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