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This static aeroelasticity project helps you to exercise your knowledge of wing divergence, aileron effectiveness/reversal and wing loading in design of a wing model. The
This static aeroelasticity project helps you to exercise your knowledge of wing divergence, aileron effectiveness/reversal and wing loading in design of a wing model. The model is a cantilever wing with span s, and chord c(y) which varies in spanwise direction as shown in the following planform
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Engineering Risk Management
Authors: Genserik Meyer, Thierry, Reniers
3rd Edition
311066531X, 978-3110665314
