Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension
Resource Information
The work Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension represents a distinct intellectual or artistic creation found in University of Missouri-St. Louis Libraries. This resource is a combination of several types including: Work, Language Material, Books.
The Resource
Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension
Resource Information
The work Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension represents a distinct intellectual or artistic creation found in University of Missouri-St. Louis Libraries. This resource is a combination of several types including: Work, Language Material, Books.
- Label
- Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension
- Statement of responsibility
- Marshall Rouse [and others]
- Language
- eng
- Cataloging source
- GPO
- Government publication
- federal national government publication
- Index
- no index present
- Literary form
- non fiction
- Series statement
- NASA/TM
- Series volume
- 208191
Context
Context of Response of composite fuselage sandwich side panels subjected to internal pressure and axial tensionWork of
No resources found
No enriched resources found
Embed
Settings
Select options that apply then copy and paste the RDF/HTML data fragment to include in your application
Embed this data in a secure (HTTPS) page:
Layout options:
Include data citation:
<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.umsl.edu/resource/jfp-lm0O6OY/" typeof="CreativeWork http://bibfra.me/vocab/lite/Work"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/jfp-lm0O6OY/">Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>
Note: Adjust the width and height settings defined in the RDF/HTML code fragment to best match your requirements
Preview
Cite Data - Experimental
Data Citation of the Work Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension
Copy and paste the following RDF/HTML data fragment to cite this resource
<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.umsl.edu/resource/jfp-lm0O6OY/" typeof="CreativeWork http://bibfra.me/vocab/lite/Work"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/jfp-lm0O6OY/">Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>