The influence of grid parameters variable over height on the weight of cylindrical and conical lattice shells made of carbon fiber is studied using the ANSYS software. The shells are loaded with longitudinal compressive and shear forces on the upper end face.
Numerical Estimation of Weight Efficiency for Aircraft Composite Lattice Shells with Grid Parameter Variable over Height
Russ. Aeronaut.
Russian Aeronautics ; 62 , 1 ; 1-4
2019-01-01
4 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Parameter Estimation for Over-Actuated Aircraft with Nonlinear Aerodynamics
British Library Conference Proceedings | 1999
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