Вплив компонування аеродинамічних профілів на аеродинамічні коефіцієнти БПЛА для великих кутів атаки
DOI:
https://doi.org/10.18372/1990-5548.86.20565Ключові слова:
cистема керування рухом, аеродинамічні коефіцієнти, експериментальне випробування, аеродинамічна труба, компонування аеродинамічного профілю, кут атакиАнотація
У статті досліджується вплив компонування аеродинамічних профілів на аеродинамічні коефіцієнти при великих кутах атаки. Наведено огляд попередніх досліджень з досліджуваної теми. Описано характеристики експериментального обладнання, включаючи набір датчиків аеродинамічного балансу та інформаційно-вимірювальну систему. Характеристики описаного експериментального обладнання дозволяють реалізувати автоматизацію експериментального випробування. Наведено основні особливості методики експерименту. Перелічено основні функції інформаційно-вимірювальної системи. Результати експериментального випробування представлені у вигляді графічних залежностей аеродинамічних коефіцієнтів від кутів атаки. Проведено детальний аналіз отриманих результатів. Результати дослідження можуть бути корисними для проектування систем керування рухом БПЛА та моделювання руху БПЛА з урахуванням аеродинамічних збурень.
Посилання
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