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Strain gage load calibration of the wing interface fittings for the adaptive compliant trailing edge flap flight test (Document No: 20140011429)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Miller, Eric J. Holguin, Andrew C. Lokos, William A. Cruz, Josue |
| Copyright Year | 2014 |
| Description | This is the presentation to follow conference paper of the same name. The adaptive compliant trailing edge (ACTE) flap experiment safety of flight requires that the flap to wing interface loads be sensed and monitored in real time to ensure that the wing structural load limits are not exceeded. This paper discusses the strain gage load calibration testing and load equation derivation methodology for the ACTE interface fittings. Both the left and right wing flap interfaces will be monitored and each contains four uniquely designed and instrumented flap interface fittings. The interface hardware design and instrumentation layout are discussed. Twenty one applied test load cases were developed using the predicted in-flight loads for the ACTE experiment. |
| File Size | 1124138 |
| Page Count | 23 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20140011429 |
| Archival Resource Key | ark:/13960/t4km49774 |
| Language | English |
| Publisher Date | 2014-01-13 |
| Access Restriction | Open |
| Subject Keyword | Strain Gage Calibration Real Time Load Monitoring Finite Element Method Loads Calibration Giii Compliant Structure Flight Tests Bending Moments Calibrating Shear Strength Mechanical Properties Axial Loads Strain Gages Trailing Edge Flaps Loads Forces Load Tests Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Presentation |
