Bottom drag measurements in experimental wind tunnel tests

نویسندگان

چکیده

Abstract The paper presents the results of wind tunnel tests aimed at determining model bottom drag in case rocket tests. balance measurement technique fixed test section by rear sting was discussed. equipped with two parallel boosters. Based on twin values pressure determined for tested Mach numbers. An algorithm corrections shown, which allowed total determination a active or passive flight. showed necessity measurements

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ژورنال

عنوان ژورنال: Journal of physics

سال: 2022

ISSN: ['0022-3700', '1747-3721', '0368-3508', '1747-3713']

DOI: https://doi.org/10.1088/1742-6596/2367/1/012001