wiki_heat-transfer_and_pressure_measurements_from_a_flight_test_of_the_third_1_18-scale_model_of_the_titan_intercontinental_ballistic_missile_up_to_a_mach_number_of_3.86_and_reynolds_number_per_foot_of_23.5_x_10_exp_6_and_a_comparison_with_heat_transfer
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