کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
8057951 | 1520058 | 2018 | 13 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Separation control by a microfabricated SDBD plasma actuator for small engine turbine applications: influence of the excitation waveform
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کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه
سایر رشته های مهندسی
مهندسی هوافضا
پیش نمایش صفحه اول مقاله
![عکس صفحه اول مقاله: Separation control by a microfabricated SDBD plasma actuator for small engine turbine applications: influence of the excitation waveform Separation control by a microfabricated SDBD plasma actuator for small engine turbine applications: influence of the excitation waveform](/preview/png/8057951.png)
چکیده انگلیسی
Velocity results showed that the extension of the separation area was reduced by actuation. Moreover, when the actuator was on, the boundary layer thickness and the negative velocity magnitude decreased. Their reduction increased with the applied voltage (i.e. higher power dissipations). At comparable peak-to-peak applied voltages, the sinus waveforms slightly outperformed the other waveforms; however, while the sinus and triangle ones had comparable power dissipation, the square wave always dissipated the most.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Aerospace Science and Technology - Volume 76, May 2018, Pages 442-454
Journal: Aerospace Science and Technology - Volume 76, May 2018, Pages 442-454
نویسندگان
E. Pescini, M.G. De Giorgi, A. Suma, L. Francioso, A. Ficarella,