Strip distortion generator for simulating inlet flow distortion in gas turbine engine ground test facilities
A methodology has been developed to generate a non-uniform/distorted inlet flow field to test a gas turbine engine in ground test facilities. The distorted flow field is generated by positioning radial and circumferential strips of varying widths upstream of the Aerodynamic Interface Plane. The inte...
| Päätekijät: | , , |
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| Aineistotyyppi: | Artikkeli |
| Kieli: | English |
| Julkaistu: |
KeAi Communications Co., Ltd.
2016-12-01
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| Sarja: | Propulsion and Power Research |
| Aiheet: | |
| Linkit: | http://www.sciencedirect.com/science/article/pii/S2212540X16300402 |