Engineering, 04.12.2019 00:31 savannaflorian5141
In example 5.1, an expression for the aspect ratio of a delta wing was developed in terms of the leading-edge sweep angle (le). for this problem, develop an expression for the aspect ratio in terms of the sweep angle of the quarter chord (c> 4).
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In example 5.1, an expression for the aspect ratio of a delta wing was developed in terms of the lea...
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