Advanced Flight Analysis of SHEFEX-I
| Autor: | Tarik Barth, Jose M. A. Longo |
|---|---|
| Jazyk: | němčina |
| Rok vydání: | 2010 |
| Předmět: |
Hyperschall
Materials science SHEFEX Numerik business.industry Heat flux sensor Wiedereintritt facettiertes Thermalschutzsystem Edge (geometry) Experiment Thermocouple Position (vector) Space Shuttle thermal protection system Range (aeronautics) scharfkantig Contact condition Aerospace engineering business Space vehicle Simulation |
| Zdroj: | Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783642142420 |
| Popis: | The first SHarp Edge Flight EXperiment of DLR has been established to demonstrate the feasibility of space vehicles with facetted Thermal Protection System (TPS). This study presents the thermodynamic behaviour of SHEFEX-I during the re-entry flight range of 60 km down to 20 km using a multidisciplinary simulation. Major effects like influence of the thermocouple position, overhang of the glue, and contact condition between the heat flux sensor and the TPS are analysed. The results of numerical calculations agree well with the experimental data. |
| Databáze: | OpenAIRE |
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