کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
5472941 | 1520066 | 2017 | 11 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
CFD simulation of flow around angle of attack and sideslip angle vanes on a BAe Jetstream 3102 - Part 2
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موضوعات مرتبط
مهندسی و علوم پایه
سایر رشته های مهندسی
مهندسی هوافضا
پیش نمایش صفحه اول مقاله
![عکس صفحه اول مقاله: CFD simulation of flow around angle of attack and sideslip angle vanes on a BAe Jetstream 3102 - Part 2 CFD simulation of flow around angle of attack and sideslip angle vanes on a BAe Jetstream 3102 - Part 2](/preview/png/5472941.png)
چکیده انگلیسی
A previous study analysing the local flow around angle of attack and sideslip angle vanes on a BAe Jetstream 3102 turboprop is extended to study the additional effects of bank angle. A full matrix of CFD simulations is carried out to investigate how the introduction of a bank angle affects vane performance for a range of flight conditions. An updated calibration method to convert the raw vane readings into true values of angle of attack and sideslip, incorporating a correction factor as a function of the bank angle, is presented. The results are shown to be accurate for a wide range of flight configurations. Uncertainty analysis indicates that raw vanes reading errors should be below ±0.1° to ensure that total calibration errors are restricted to less than 2% for angle of attack and 5% for sideslip angle.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Aerospace Science and Technology - Volume 68, September 2017, Pages 577-587
Journal: Aerospace Science and Technology - Volume 68, September 2017, Pages 577-587
نویسندگان
C.J. Bennett, N.J. Lawson, J.E. Gautrey, A. Cooke,