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A concept of waveriding dependent area (WDA) is proposed by referring to the theory of characteristics to determine the shock-dependent flow area, and the waverider only retaining WDA was able to maintain the shock strength and therefore waveriding performance.
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This page is a summary of: Theory, Method, and Analysis of Waveriding-Dependent Area, AIAA Journal, June 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j065024.
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