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- W2351888567 abstract "The loads calibration test of aircraft wing is one of the crucial works of the loads validation flight test.The testing accuracy and validity mainly depend on the rationality of the test scheme design.In order to research it through simulating,the method of simulating the loads calibration test of aircraft wing using finite element method (FEM) was studied.Some critical technologies of building the finite element model for this simulation and designing virtual strain-gage and applying the virtual calibration load were established.Based on them,an example of a wing calibration test simulation was given,and comparison and evaluation of its result were done.The conclusion shows the method has an approving precision and is feasible." @default.
- W2351888567 created "2016-06-24" @default.
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- W2351888567 date "2008-01-01" @default.
- W2351888567 modified "2023-09-23" @default.
- W2351888567 title "Technology of FEM Simulation in Aircraft Wing Loads Calibration Test" @default.
- W2351888567 hasPublicationYear "2008" @default.
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