王云, 刘伟. 风扇增升机翼[J]. 南昌航空大学学报(自然科学版), 2010, 24(4): 38-42.
引用本文: 王云, 刘伟. 风扇增升机翼[J]. 南昌航空大学学报(自然科学版), 2010, 24(4): 38-42.
WANG Yun, LIU Wei. Fan Higher Lift Wing[J]. Journal of nanchang hangkong university(Natural science edition), 2010, 24(4): 38-42.
Citation: WANG Yun, LIU Wei. Fan Higher Lift Wing[J]. Journal of nanchang hangkong university(Natural science edition), 2010, 24(4): 38-42.

风扇增升机翼

Fan Higher Lift Wing

  • 摘要: 文章首先提出了利用推力风扇制造的低压区来增大机翼升力的增升机翼方案.然后,对风扇位于翼型不同位置的多种方案进行了分析,并使用fluent进行数值模拟实验验证得出风扇在翼型上方能增大机翼升力.当风扇后置时机翼的升力增加最大,但其阻力也有所增加.当风扇前置时机翼升力增加的同时阻力也有所减小,在这种情况下机翼的升阻比明显增大.风扇前置和后置方法各有其不同的优点,可以根据不同场合的要求分别应用.

     

    Abstract: This article first puts forward a program of higher lift wing by using the thrusting fan's low pressure to increase the wing's lift.The program does not require specialized installation of lift device.It just needs putting the thrusting fan on right place above the wing.So this is a program of combination of lift and thrust to get higher lift.The paper has analyzed several programs that put the fan on the different place of the wing,and got conclusions that when the fan is above the wing,it increases wing's lift through using the fluent to do the numerical simulation experiments.It is noted that when the fan is put on back of wing it increases the wing's lift and wing's drag.When the fan is put on front of wing,it not only increases wing's lift,but reduces wing's drag,and in this case the wing's lift-drag ratio has increased significantly.Putting the fan on the back of the wing and on the front of the wing has different advantages,we can use it in different occasions according to the requirements of the respective applications on different occasions.

     

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