Research on Distributed Jet Blowing Wing Based on the Principle of Fan-Wing Vortex-Induced Lift and Thrust

المؤلفون المشاركون

Siliang, Du
Qijun, Zhao
Bo, Wang

المصدر

International Journal of Aerospace Engineering

العدد

المجلد 2019، العدد 2019 (31 ديسمبر/كانون الأول 2019)، ص ص. 1-11، 11ص.

الناشر

Hindawi Publishing Corporation

تاريخ النشر

2019-07-09

دولة النشر

مصر

عدد الصفحات

11

الملخص EN

Based on the numerical calculation and analysis of the principle of the lift and thrust of the Fan-wing.

A new scheme for the wing of Fan-wing aircraft-distributed jet blowing wing was presented.

Firstly, the mechanism of the formation process of the vortex-induced lift and thrust force of the two kinds of wings was analyzed.

Then, the numerical calculation method and validation example were verified.

It was proved that the distributed jet blowing wing had the same vortex-induced lift and thrust mode as that of the Fan-wing by comparing the relative static pressure distribution curve, velocity contours, and pressure contours.

Finally, the blow-up speed of a jet blowing wing was defined and the relationship between the lift and thrust of two wings with the flow speed and angle of attack was compared.

The result indicated that the lift and thrust of the distributed jet blowing wing was similar to those of the Fan-wing under normal flight conditions.

Therefore, it was proved that the Fan-wing can be replaced by the distributed jet blowing wing.

Furthermore, distributed jet blowing wing technology has the potential value for application in an ultrashort take-off and landing concept aircraft.

نمط استشهاد جمعية علماء النفس الأمريكية (APA)

Siliang, Du& Qijun, Zhao& Bo, Wang. 2019. Research on Distributed Jet Blowing Wing Based on the Principle of Fan-Wing Vortex-Induced Lift and Thrust. International Journal of Aerospace Engineering،Vol. 2019, no. 2019, pp.1-11.
https://search.emarefa.net/detail/BIM-1156933

نمط استشهاد الجمعية الأمريكية للغات الحديثة (MLA)

Siliang, Du…[et al.]. Research on Distributed Jet Blowing Wing Based on the Principle of Fan-Wing Vortex-Induced Lift and Thrust. International Journal of Aerospace Engineering No. 2019 (2019), pp.1-11.
https://search.emarefa.net/detail/BIM-1156933

نمط استشهاد الجمعية الطبية الأمريكية (AMA)

Siliang, Du& Qijun, Zhao& Bo, Wang. Research on Distributed Jet Blowing Wing Based on the Principle of Fan-Wing Vortex-Induced Lift and Thrust. International Journal of Aerospace Engineering. 2019. Vol. 2019, no. 2019, pp.1-11.
https://search.emarefa.net/detail/BIM-1156933

نوع البيانات

مقالات

لغة النص

الإنجليزية

الملاحظات

Includes bibliographical references

رقم السجل

BIM-1156933