<?xml version="1.0" encoding="UTF-8"?>
<!DOCTYPE ArticleSet PUBLIC "-//NLM//DTD PubMed 2.7//EN" "https://dtd.nlm.nih.gov/ncbi/pubmed/in/PubMed.dtd">
<ArticleSet>
<Article>
<Journal>
				<PublisherName>Amirkabir University of Technology</PublisherName>
				<JournalTitle>AUT Journal of Mechanical Engineering</JournalTitle>
				<Issn>2588-2937</Issn>
				<Volume>10</Volume>
				<Issue>4</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>10</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Vibration Analysis of Open Spherical Sandwich Panels with Soft Core Rested on an Elastic Foundation Subjected to Various Impulse Loads</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage></FirstPage>
			<LastPage></LastPage>
			<ELocationID EIdType="pii">6032</ELocationID>
			
<ELocationID EIdType="doi">10.22060/ajme.2026.24389.6200</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Saman</FirstName>
					<LastName>Sadripour</LastName>
<Affiliation>School of Mechanical Engineering, Babol Noshirvani University of Technology, Babol, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Raed Hadi</FirstName>
					<LastName>Al Saffah</LastName>
<Affiliation>School of Mechanical Engineering, Babol Noshirvani University of Technology, Babol, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Ramazan-Ali</FirstName>
					<LastName>Jafari-Talookolaei</LastName>
<Affiliation>School of Mechanical Engineering, Babol Noshirvani University of Technology, Babol, Iran</Affiliation>
<Identifier Source="ORCID">0000-0003-4357-2597</Identifier>

</Author>
<Author>
					<FirstName>Reza</FirstName>
					<LastName>Azadi</LastName>
<Affiliation>School of Mechanical Engineering, Babol Noshirvani University of Technology, Babol, Iran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2025</Year>
					<Month>07</Month>
					<Day>23</Day>
				</PubDate>
			</History>
		<Abstract>The study explores the behaviour of systems under both free and forced vibrations of spherical sandwich panels supported by an elastic foundation exposed to various impact load profiles. The panels consist of multilayer composite face sheets formulated based on the first-order shear deformation theory, and a soft core characterized by a higher-order theory employing third-order in-plane and second-order transverse displacement fields. By calculating the mechanical energy components, and introducing a higher-order element with nine nodes and 15 degrees of freedom for each node, the element stiffness and mass matrices were determined. Boundary conditions are simulated through distributed virtual springs. A free vibration problem is evaluated to extract the structure’s natural frequencies and mode shapes. Using the Newmark method, time response of displacement, velocity, acceleration, and phase planes are calculated for various impact profiles, specifically for half-sine pulses. This comprehensive analysis of sandwich panels&#039; dynamic response under various impact loads reveals that the load profile critically determines structural behavior, essentially governing the boundary between safe operation and potential failure. For example, sudden loads like rectangular pulse emerged as the most critical case, causing extreme discontinuous responses across all dynamic parameters, and gradual loads (Gaussian/exponential) proved optimal for sensitive applications by generating smooth, controlled structural responses and providing ideal performance for stability-critical systems.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">free vibration</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Transient Response</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Sandwich Shell</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Soft-Core</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Finite Element Method (FEM)</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://ajme.aut.ac.ir/article_6032_fb3a30a2e3e8abdcbf63f0aaaadb06e4.pdf</ArchiveCopySource>
</Article>
</ArticleSet>
