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Regarding the latter, the error source in the steady integral panel method is discussed.
During the study, the control equation of the steady integral panel method for CRP is derived in detail.
Based on this analysis, an integral panel method for HCRSP propulsor is developed and the wake model discussed.
From the experience of developing an integral panel method for CRP, the characteristics of panel singularity strength in HCRSP propulsor was analyzed.
Comparison between experimental data and numerical results shows that the steady integral panel method has good accuracy in terms of open water performance.
Nowadays, more and more attentions are paid to electromagnetic incremental forming (EMIF), especially for a part with a large-scale size, e.g., an integral panel with stiffened ribs.
Similar(50)
In order to design the press bend forming path of aircraft integral panels, a novel optimization method was proposed, which integrates FEM equivalent model based on previous study, the artificial neural network response surface, and the genetic algorithm.
The results obtained in this work are useful for forming integral panels with stiffened ribs via the EMIF process.
The plastic equivalent model is valuable and essential for the further research on the press bend forming process of large scale complicated integral panels.
With the proposed method, the buckling of the stiffeners in press bend forming of the aluminum alloy integral panels with high-stiffener can be predicted reasonably.
Aluminum alloy high-stiffener integral panels are widely used on modern aircrafts to meet the demand of light weight and high stiffness.
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