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Titanium honeycomb panel testing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Thompson, Randolph C. Richards, W. Lance |
| Copyright Year | 1996 |
| Description | Thermal-mechanical tests were performed on a titanium honeycomb sandwich panel to experimentally validate the hypersonic wing panel concept and compare test data with analysis. Details of the test article, test fixture development, instrumentation, and test results are presented. After extensive testing to 900 deg. F, non-destructive evaluation of the panel has not detected any significant structural degradation caused by the applied thermal-mechanical loads. |
| File Size | 1098661 |
| Page Count | 22 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19970002982 |
| Archival Resource Key | ark:/13960/t38101g3k |
| Language | English |
| Publisher Date | 1996-10-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Hypersonics Nondestructive Tests Fixtures Mechanical Properties Titanium Strain Gages Honeycomb Structures Wing Panels Hypersonic Vehicles Loads Forces Structural Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
