The Aerodynamic Behavioral Study of Tandem Fan Wing Configuration

المؤلفون المشاركون

Siliang, Du
Zhengfei, Tang

المصدر

International Journal of Aerospace Engineering

العدد

المجلد 2018، العدد 2018 (31 ديسمبر/كانون الأول 2018)، ص ص. 1-14، 14ص.

الناشر

Hindawi Publishing Corporation

تاريخ النشر

2018-10-30

دولة النشر

مصر

عدد الصفحات

14

الملخص EN

The fan wing aircraft is a new concept based on a new principle, especially its wing which is based on a unique aerodynamic principle.

A fan wing can simultaneously generate lift and thrust.

In order to further improve its aerodynamic characteristics without changing its basic geometric parameters, two fan wings are installed along the longitudinal body, which is the composition of a tandem fan wing aircraft.

Through numerical simulation, the lift and thrust of the fan wings were calculated with the distance, height, and installation angle of the front and rear fan wings changed, and the aerodynamic characteristic interaction rule between the front and rear fan wings was analyzed.

In addition, the wind test model of a tandem fan wing was designed, and the results of the wind tunnel test and numerical calculation results were compared to verify the preliminary setup.

The results show that at a certain height, distance, and installation angle, aerodynamic characteristics of a tandem fan wing have more advantages compared to the single fan wing.

Therefore, the tandem fan wing aircraft’s advantages have good prospects for development and application.

نمط استشهاد جمعية علماء النفس الأمريكية (APA)

Siliang, Du& Zhengfei, Tang. 2018. The Aerodynamic Behavioral Study of Tandem Fan Wing Configuration. International Journal of Aerospace Engineering،Vol. 2018, no. 2018, pp.1-14.
https://search.emarefa.net/detail/BIM-1166718

نمط استشهاد الجمعية الأمريكية للغات الحديثة (MLA)

Siliang, Du& Zhengfei, Tang. The Aerodynamic Behavioral Study of Tandem Fan Wing Configuration. International Journal of Aerospace Engineering No. 2018 (2018), pp.1-14.
https://search.emarefa.net/detail/BIM-1166718

نمط استشهاد الجمعية الطبية الأمريكية (AMA)

Siliang, Du& Zhengfei, Tang. The Aerodynamic Behavioral Study of Tandem Fan Wing Configuration. International Journal of Aerospace Engineering. 2018. Vol. 2018, no. 2018, pp.1-14.
https://search.emarefa.net/detail/BIM-1166718

نوع البيانات

مقالات

لغة النص

الإنجليزية

الملاحظات

Includes bibliographical references

رقم السجل

BIM-1166718