Objective: Test a C/SiC Ruddervator Subcomponent under relevant thermal, mechanical & dynamic loading a) Thermal-structural mission cycling for re-entry and hypersonic cruise conditions; b) High-temperature modal survey to study the effect of heating on mode shapes, natural frequencies and damping. Supports NASA ARMD Hypersonics Material & Structures Program. Partners: NASA Dryden / Langley / Glenn, Lockheed-Martin, Materials Research & Design, GE CCP Test Phases - Phase 1: Acoustic-Vibration Testing (LaRC) completed - Phase 2: Thermal-Mechanical Testing (DFRC) in assembly - Phase 3: Mechanical Testing (DFRC) in assembly
10.2 Thermal-Structural Testing
2008
33 pages
Report
Keine Angabe
Englisch
10.2 Thermal-Structural Testing
NTRS | 2008
|Aerospace thermal-structural testing technology
Tema Archiv | 1997
|British Library Conference Proceedings | 2009
|MOIRE Thermal Vacuum Structural Stability Testing
AIAA | 2015
|