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High-speed t-38a landing gear extension loads
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Schmitt, A. L. |
| Copyright Year | 1980 |
| Description | Testing of T-38A landing gear extension at high speed and high altitude is described. The mechanisms are shown together with peak hydraulic pressure data during landing gear deployment with active and inactive strut door flaps. Results of strain gage measurements of stress on various structural members are included. |
| File Size | 491824 |
| Page Count | 22 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800016824 |
| Archival Resource Key | ark:/13960/t29931v9b |
| Language | English |
| Publisher Date | 1980-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Flight Tests High Altitude Stress Analysis Landing Gear High Speed Strain Gages Hydraulic Equipment Aerodynamic Forces T-38 Aircraft Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
