Structural influence coefficients were calculated for various wing planforms using the KU Aeroelastic and NASTRAN programs. The resulting matrices are compared with experimental results. Conclusions are given.
An analytical study of effects of aeroelasticity on control effectiveness
1975-12-01
Report
No indication
English
FLIGHT VEHICLE AEROELASTICITY - Nonlinear Aeroelasticity
Online Contents | 2003
|NTIS | 2021
|NTRS | 1970
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