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A detailed comparison of resu[ts has been made from several series of flight tests, spanning a number of years, on the Fairey Delta 2, with wind tunnel tests on 1/9 and 1/24 scale models and with reference also to simple theoretical results. The Mach number range of interest has been M = 0.6 to M = 1.8. This report considers both longitudinal and lateral(More)
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