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Fatigue tests on big structure assemblies of concorde aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Perrais, J. P. Nguyen, V. P. |
| Copyright Year | 1972 |
| Description | Fatigue tests on structural assemblies of the Concorde supersonic transport aircraft are reported. Two main sections of the aircraft were subjected to pressure, mechanical load, and thermal static tests. The types of fatigue tests conducted and the results obtained are discussed. It was concluded that on a supersonic aircraft whose structural weight is a significant part of the weight analysis, many fatigue and static strength development tests should be made and fatigue and thermal tests of the structures are absolutely necessary. |
| File Size | 940859 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720022265 |
| Archival Resource Key | ark:/13960/t5t775j2w |
| Language | English |
| Publisher Date | 1972-01-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Fatigue Tests Structural Stability Airframes High Temperature Tests Structural Reliability Concorde Aircraft Static Tests 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 |
