{"id":352,"date":"2025-06-25T05:08:39","date_gmt":"2025-06-25T05:08:39","guid":{"rendered":"https:\/\/sutrasys.com\/Falcon\/?page_id=352"},"modified":"2026-03-27T09:16:22","modified_gmt":"2026-03-27T09:16:22","slug":"laminar_composite_plate","status":"publish","type":"page","link":"https:\/\/sutrasys.com\/Falcon\/laminar_composite_plate\/","title":{"rendered":"Laminar_Composite_Plate"},"content":{"rendered":"\n
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Laminar Composite Plate<\/a><\/h2>\n<\/div>\n<\/div>\n<\/div>\n<\/div>\n\n\n\n
    \n
  • Structural behaviour of a Laminar Composite Plate<\/li>\n\n\n\n
  • The following model is solved using MyStran solver<\/strong>.<\/li>\n<\/ul>\n\n\n\n
    Objective<\/summary>\n

    Study the structural response of a three-layer cross-ply laminated composite plate under uniform normal pressure 100 psi.<\/p>\n\n\n\n

    \n

    The figure below shows three plates laminated with cross layers (“cross-ply”).<\/p>\n\n\n\n

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    \"\"<\/figure>\n<\/div>\n\n\n\n
    \n

    <\/p>\n<\/div>\n\n\n\n

    <\/div>\n<\/div>\n<\/div>\n<\/details>\n\n\n\n
    1. Define Geometry<\/summary>\n

    Study the structural response of a three-layer cross-ply laminated composite plate under uniform normal pressure 100 psi.<\/p>\n\n\n\n

    \n

    The figure below shows three plates laminated with cross layers (“cross-ply”).<\/p>\n\n\n\n

    \n
    \n
    Parameter<\/td>Value<\/td><\/tr>
    Plate defined by points<\/td>(0,0,0), (5,0,0), (5,5,0), (0,5,0)<\/td><\/tr>
    Width ( X )<\/td>5 inch<\/td><\/tr>
    Width ( Y )<\/td>5 inch<\/td><\/tr>
    Face Sheet Thickness<\/td>0.028 inch<\/td><\/tr>
    Core Thickness<\/td>0.750 inch<\/td><\/tr><\/tbody><\/table><\/figure>\n<\/div>\n\n\n\n
    \n
    \"\"<\/figure>\n<\/div>\n<\/div>\n<\/div>\n<\/details>\n\n\n\n
    2. Define Material<\/summary>\n

    Study the structural response of a three-layer cross-ply laminated composite plate under uniform normal pressure 100 psi.<\/p>\n\n\n\n

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    Material 1 : Laminar_Facesheet<\/p>\n\n\n\n

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    \n
    Parameter<\/td>Value<\/td><\/tr>
    Mass Density<\/td>1E-04 lbf-sec2<\/sup>\/in4<\/sup><\/td><\/tr>
    Young\u2019s Modulus X (E1)Young\u2019s Modulus X (E1)<\/td>1E7 psi<\/td><\/tr>
    Young\u2019s Modulus Y (E2)<\/td>4E6 psi<\/td><\/tr>
    Poisson\u2019s Ratio X (nu12)<\/td>0.3<\/td><\/tr>
    Shear Modulus X (G12)<\/td>1,875E6 psi<\/td><\/tr>
    Shear Modulus Y (G13)<\/td>1,875E6 psi<\/td><\/tr>
    Shear Modulus Z (G23)<\/td>1,875E6 psi<\/td><\/tr><\/tbody><\/table><\/figure>\n<\/div>\n\n\n\n
    <\/div>\n<\/div>\n\n\n\n

    Material 2 : Laminar_Core<\/p>\n\n\n\n

    \n
    \n
    Parameter<\/td>Value<\/td><\/tr>
    Mass Density<\/td>1E-04 lbf-sec2<\/sup>\/in4<\/sup><\/td><\/tr>
    Young\u2019s Modulus X (E1)<\/td>10 psi<\/td><\/tr>
    Young\u2019s Modulus Y (E2)<\/td>10 psi<\/td><\/tr>
    Poisson\u2019s Ratio X (nu12)<\/td>0<\/td><\/tr>
    Shear Modulus X (G12)<\/td>10 psi<\/td><\/tr>
    Shear Modulus Y (G13)<\/td>3E4 psi<\/td><\/tr>
    Shear Modulus Z (G23)<\/td>1.2E4 psi<\/td><\/tr><\/tbody><\/table><\/figure>\n<\/div>\n\n\n\n
    <\/div>\n<\/div>\n<\/div>\n<\/details>\n\n\n\n
    3. Define Property<\/summary>\n

    PCOMP property with ply properties.<\/p>\n\n\n\n

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    \"\"<\/figure>\n<\/div>\n\n\n\n
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    \"\"<\/figure>\n<\/div>\n<\/div>\n<\/div>\n<\/details>\n\n\n\n
    4. Meshing<\/summary>\n
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    \"\"<\/figure>\n\n\n\n

    Mesh Size 0.625 inch<\/p>\n<\/div>\n\n\n\n

    <\/div>\n<\/div>\n<\/div>\n<\/details>\n\n\n\n
    5. Boundary Conditions<\/summary>\n
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    \"\"<\/figure>\n<\/div>\n\n\n\n
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    \n

    Pressure normal uniform value 100 psi to all surfaces of the model<\/p>\n\n\n\n

    \"\"<\/figure>\n<\/div>\n<\/div>\n<\/div>\n<\/div>\n<\/div>\n<\/details>\n\n\n\n
    6. Static Analysis (Mystran Solver)<\/summary>\n
    \n
    \n
    \n
    \"\"<\/figure>\n<\/div>\n<\/div>\n<\/div>\n<\/details>\n\n\n\n
    7. Result<\/summary>\n
    \n
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    \n
    \n
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    \"\"<\/figure>\n<\/div>\n\n\n\n
    <\/div>\n<\/div>\n<\/div>\n<\/div>\n\n\n\n
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    \"\"<\/figure>\n<\/div>\n\n\n\n
    <\/div>\n<\/div>\n<\/div>\n<\/div>\n\n\n\n

    <\/p>\n<\/div>\n<\/details>\n<\/div>\n<\/div>\n\n\n\n

    <\/p>\n","protected":false},"excerpt":{"rendered":"

    Laminar Composite Plate<\/p>\n","protected":false},"author":2,"featured_media":0,"parent":0,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"nf_dc_page":"","om_disable_all_campaigns":false,"_monsterinsights_skip_tracking":false,"_monsterinsights_sitenote_active":false,"_monsterinsights_sitenote_note":"","_monsterinsights_sitenote_category":0,"footnotes":""},"class_list":["post-352","page","type-page","status-publish","hentry"],"yoast_head":"\nLaminar_Composite_Plate - Falcon: Cost-Effective Pre Post Processor for FEA<\/title>\n<meta name=\"robots\" content=\"index, follow, max-snippet:-1, max-image-preview:large, max-video-preview:-1\" \/>\n<link rel=\"canonical\" href=\"https:\/\/sutrasys.com\/Falcon\/laminar_composite_plate\/\" \/>\n<meta property=\"og:locale\" content=\"en_US\" \/>\n<meta property=\"og:type\" content=\"article\" \/>\n<meta property=\"og:title\" content=\"Laminar_Composite_Plate - Falcon: Cost-Effective Pre Post Processor for FEA\" \/>\n<meta property=\"og:description\" content=\"Laminar Composite Plate\" \/>\n<meta property=\"og:url\" content=\"https:\/\/sutrasys.com\/Falcon\/laminar_composite_plate\/\" \/>\n<meta property=\"og:site_name\" content=\"Falcon: Cost-Effective Pre Post Processor for FEA\" \/>\n<meta property=\"article:modified_time\" content=\"2026-03-27T09:16:22+00:00\" \/>\n<meta property=\"og:image\" content=\"https:\/\/sutrasys.com\/Falcon\/wp-content\/uploads\/2026\/02\/ThreePly.png\" \/>\n<meta name=\"twitter:card\" content=\"summary_large_image\" \/>\n<meta name=\"twitter:label1\" content=\"Est. reading time\" \/>\n\t<meta name=\"twitter:data1\" content=\"4 minutes\" \/>\n<script type=\"application\/ld+json\" class=\"yoast-schema-graph\">{\"@context\":\"https:\\\/\\\/schema.org\",\"@graph\":[{\"@type\":\"WebPage\",\"@id\":\"https:\\\/\\\/sutrasys.com\\\/Falcon\\\/laminar_composite_plate\\\/\",\"url\":\"https:\\\/\\\/sutrasys.com\\\/Falcon\\\/laminar_composite_plate\\\/\",\"name\":\"Laminar_Composite_Plate - Falcon: Cost-Effective Pre Post Processor for FEA\",\"isPartOf\":{\"@id\":\"https:\\\/\\\/sutrasys.com\\\/Falcon\\\/#website\"},\"primaryImageOfPage\":{\"@id\":\"https:\\\/\\\/sutrasys.com\\\/Falcon\\\/laminar_composite_plate\\\/#primaryimage\"},\"image\":{\"@id\":\"https:\\\/\\\/sutrasys.com\\\/Falcon\\\/laminar_composite_plate\\\/#primaryimage\"},\"thumbnailUrl\":\"https:\\\/\\\/sutrasys.com\\\/Falcon\\\/wp-content\\\/uploads\\\/2026\\\/02\\\/ThreePly.png\",\"datePublished\":\"2025-06-25T05:08:39+00:00\",\"dateModified\":\"2026-03-27T09:16:22+00:00\",\"breadcrumb\":{\"@id\":\"https:\\\/\\\/sutrasys.com\\\/Falcon\\\/laminar_composite_plate\\\/#breadcrumb\"},\"inLanguage\":\"en-US\",\"potentialAction\":[{\"@type\":\"ReadAction\",\"target\":[\"https:\\\/\\\/sutrasys.com\\\/Falcon\\\/laminar_composite_plate\\\/\"]}]},{\"@type\":\"ImageObject\",\"inLanguage\":\"en-US\",\"@id\":\"https:\\\/\\\/sutrasys.com\\\/Falcon\\\/laminar_composite_plate\\\/#primaryimage\",\"url\":\"https:\\\/\\\/i0.wp.com\\\/sutrasys.com\\\/Falcon\\\/wp-content\\\/uploads\\\/2026\\\/02\\\/ThreePly.png?fit=394%2C343&ssl=1\",\"contentUrl\":\"https:\\\/\\\/i0.wp.com\\\/sutrasys.com\\\/Falcon\\\/wp-content\\\/uploads\\\/2026\\\/02\\\/ThreePly.png?fit=394%2C343&ssl=1\",\"width\":394,\"height\":343},{\"@type\":\"BreadcrumbList\",\"@id\":\"https:\\\/\\\/sutrasys.com\\\/Falcon\\\/laminar_composite_plate\\\/#breadcrumb\",\"itemListElement\":[{\"@type\":\"ListItem\",\"position\":1,\"name\":\"Home\",\"item\":\"https:\\\/\\\/sutrasys.com\\\/Falcon\\\/\"},{\"@type\":\"ListItem\",\"position\":2,\"name\":\"Laminar_Composite_Plate\"}]},{\"@type\":\"WebSite\",\"@id\":\"https:\\\/\\\/sutrasys.com\\\/Falcon\\\/#website\",\"url\":\"https:\\\/\\\/sutrasys.com\\\/Falcon\\\/\",\"name\":\"Falcon: Cost-Effective Pre Post Processor for FEA\",\"description\":\"Discover Falcon, the cost-effective pre and post processor for Finite Element Analysis. 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