Truss core mass design analysis of cantilever bending sandwich structure with variable spanwise and chordwise dimensions
Russian aeronautics ; 57 , 4 ; 412-415
2014
Aufsatz (Zeitschrift)
Englisch
Lokalklassifikation TIB: | 770/7040/8000 | |
BKL: | 55.50 Luftfahrzeugtechnik |
Wing with trailing edge having spanwise-chordwise continuous deformation capability
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|FLUID DYNAMICS - Numerical Simulation of a Flapping Foil with Chordwise or Spanwise Flexibility
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