I am investigating a canard-tail missile. We have recently conducted a wind tunnel test of the complete configuration in Mach 0.5 to 1.4. At this stage we plan to calculate the loads on the canard panels (hinge moments etc.) with Fluent. Can someone please tell me where I can find test cases of delta wings (wing alone) in the litterature.
Re: Delta wing
(1). Delta wing is a fairly standard case, and the best place to start is the AIAA Journal. good luck.
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