Experimental and FEM Modal Analysis of a Deployable-Retractable Wing
نویسندگان
چکیده
منابع مشابه
Experimental and FEM Modal Analysis of a Deployable-Retractable Wing
The aim of this paper is to conduct experimental modal analysis and numerical simulation to verify the structural characteristics of a deployable-retractable wing for aircraft and spacecraft. A modal impact test was conducted in order to determine the free vibration characteristics. Natural frequencies and vibration mode shapes were obtained via measurement in LMS Test. Lab. The frequency respo...
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ژورنال
عنوان ژورنال: Modern Mechanical Engineering
سال: 2014
ISSN: 2164-0165,2164-0181
DOI: 10.4236/mme.2014.44018