Truss core mass design analysis of cantilever bending sandwich structure with variable spanwise and chordwise dimensions
Russian aeronautics ; 57 , 4
2014
Article (Journal)
English
BKL: | 55.50 Luftfahrzeugtechnik | |
Local classification TIB: | 770/7040/8000 |
Wing with trailing edge having spanwise-chordwise continuous deformation capability
European Patent Office | 2023
|FLUID DYNAMICS - Numerical Simulation of a Flapping Foil with Chordwise or Spanwise Flexibility
Online Contents | 2007
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