Significant errors are pointed out in accepted practice of writing aerodynamic forces and moments that act on body of revolution; more correct formulation presented shows that, even with linear aerodynamic coefficients, differential equations governing motion are fundamentally nonlinear.
Study of aerodynamic forces and moments on bodies of revolution in combined pitching and yawing motions
NASA -- Tech Note
1960
24 pages
Report
English
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Combined pitching and yawing motion of airplanes
NTRS | 1931
|Combined pitching and yawing motion of airplanes
Engineering Index Backfile | 1931
|