High-intensity acoustic tests of a thermally stressed plate
An investigation was conducted in the Thermal Acoustic Fatigue Apparatus at the Langley Research Center to study the acoustically excited random motion of an aluminum plate which is buckled due to thermal stresses. The thermal buckling displacements were measured and compared with theory. The genera...
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| Veröffentlicht in: | Journal of aircraft 1991-04, Vol.28 (4), p.275-281 |
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| container_end_page | 281 |
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| container_issue | 4 |
| container_start_page | 275 |
| container_title | Journal of aircraft |
| container_volume | 28 |
| creator | Ng, Chung Fai Clevenson, Sherman A |
| description | An investigation was conducted in the Thermal Acoustic Fatigue Apparatus at the Langley Research Center to study the acoustically excited random motion of an aluminum plate which is buckled due to thermal stresses. The thermal buckling displacements were measured and compared with theory. The general trends of the changes in resonances frequencies and random responses of the plate agree with previous theoretical prediction and experimental results for a mechanically buckled plate. |
| doi_str_mv | 10.2514/3.46023 |
| format | Article |
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The thermal buckling displacements were measured and compared with theory. 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The thermal buckling displacements were measured and compared with theory. The general trends of the changes in resonances frequencies and random responses of the plate agree with previous theoretical prediction and experimental results for a mechanically buckled plate.</description><subject>Acoustics</subject><subject>Exact sciences and technology</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Physics</subject><subject>Solid mechanics</subject><subject>Structural and continuum mechanics</subject><subject>Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)</subject><issn>0021-8669</issn><issn>1533-3868</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1991</creationdate><recordtype>article</recordtype><sourceid>CYI</sourceid><recordid>eNqNkEtLAzEUhYMoWKv4B1zMQhQXU5PJYxJciagVCm50He6kGTslnam5Kdh_79T6QFeu7uJ-nPNxCDlmdFRIJi75SCha8B0yYJLznGuld8mA0oLlWimzTw4Q55RSTctyQK7Gzcssb9rkW2zSOgPXrTA1LkseE2ZdnUGWZj4uIIR1hil6RD_NlgGSPyR7NQT0R593SJ7vbp9uxvnk8f7h5nqSAzc65RUtNTBeytopB6VkMK20llOvfMGrQmwMDasqVlIqtCilAcNAU6qEE1JVfEjOtrnL2L2uei-7aND5EKD1va0thFFFqYr_gNIIpXvwfAu62CFGX9tlbBYQ15ZRu1nRcvuxYk-efkYCOgh1hNY1-I0L00f2Ow_JyRZrAcG2KaJlxjBKpZTG9O-L7RsaADvvVrHtB_sqsctpbetVCMm_pZ_G3-xfsXfklZEy</recordid><startdate>19910401</startdate><enddate>19910401</enddate><creator>Ng, Chung Fai</creator><creator>Clevenson, Sherman A</creator><general>American Institute of Aeronautics and Astronautics</general><scope>CYE</scope><scope>CYI</scope><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope><scope>7QF</scope><scope>8BQ</scope><scope>JG9</scope></search><sort><creationdate>19910401</creationdate><title>High-intensity acoustic tests of a thermally stressed plate</title><author>Ng, Chung Fai ; Clevenson, Sherman A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a398t-b078a1375fc6ca751adb885de6e23b24386891bb1700484759a91a80064c456b3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1991</creationdate><topic>Acoustics</topic><topic>Exact sciences and technology</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Physics</topic><topic>Solid mechanics</topic><topic>Structural and continuum mechanics</topic><topic>Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Ng, Chung Fai</creatorcontrib><creatorcontrib>Clevenson, Sherman A</creatorcontrib><collection>NASA Scientific and Technical Information</collection><collection>NASA Technical Reports Server</collection><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Aluminium Industry Abstracts</collection><collection>METADEX</collection><collection>Materials Research Database</collection><jtitle>Journal of aircraft</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Ng, Chung Fai</au><au>Clevenson, Sherman A</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>High-intensity acoustic tests of a thermally stressed plate</atitle><jtitle>Journal of aircraft</jtitle><date>1991-04-01</date><risdate>1991</risdate><volume>28</volume><issue>4</issue><spage>275</spage><epage>281</epage><pages>275-281</pages><issn>0021-8669</issn><eissn>1533-3868</eissn><coden>JAIRAM</coden><abstract>An investigation was conducted in the Thermal Acoustic Fatigue Apparatus at the Langley Research Center to study the acoustically excited random motion of an aluminum plate which is buckled due to thermal stresses. 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| fulltext | fulltext |
| identifier | ISSN: 0021-8669 |
| ispartof | Journal of aircraft, 1991-04, Vol.28 (4), p.275-281 |
| issn | 0021-8669 1533-3868 |
| language | eng |
| recordid | cdi_nasa_ntrs_19910055599 |
| source | NASA Technical Reports Server; Alma/SFX Local Collection |
| subjects | Acoustics Exact sciences and technology Fundamental areas of phenomenology (including applications) Physics Solid mechanics Structural and continuum mechanics Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...) |
| title | High-intensity acoustic tests of a thermally stressed plate |
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