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- W2037938284 abstract "An evaluation is made of six diverse examples of nonlinear treatments of slender body theory for the prediction of missile aerodynamic behavior. The cases in question are the application of area rule to store carriage design in the drag rise region, the estimation of destabilizing pitching moments associated with transonic projectiles, the pressure loadings on elliptical missile airframes, nonlinear control characteristics, roll control effectiveness in canard missile configurations, and novel approaches for vortex flow modeling." @default.
- W2037938284 created "2016-06-24" @default.
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- W2037938284 date "1985-08-17" @default.
- W2037938284 modified "2023-09-25" @default.
- W2037938284 title "Nonlinear applications of slender-body theory to missile aerodynamics" @default.
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- W2037938284 doi "https://doi.org/10.2514/6.1985-1775" @default.
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