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Paper Information

Journal:   JOURNAL OF APPLIED FLUID MECHANICS (JAFM)   2016 , Volume 9 , Number 6; Page(s) 2993 To 3000.
 
Paper: 

EFFECT OF ADVANCE RATIO AND BLADE PLANFORM ON THE PROPELLER PERFORMANCE OF A HIGH ALTITUDE AIRSHIP

 
 
Author(s):  LIU Z., LIU P.*, QU Q., HU T.
 
* BEIJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS, BEIJING, 100191, CHINA
 
Abstract: 

Experimental investigations on the influences of Reynolds number, blade planform and advance ratio on the aerodynamic performance are carried. Different from conventional aircraft propellers, the HAA propellers are characterized by low Reynolds number, large thrust requirement and low advance ratio. At the moment, the theoretical guidance and industrial experience in designing such propellers are still lacked. In the present study, the influence of Reynolds number is firstly studied via tests of a propeller at different rotational speeds. It is found that, for the propeller with airfoil S1223, the influence of Reynolds number is negligible as...

 
Keyword(s): HIGH ALTITUDE AIRSHIP PROPELLER, BLADE PLANFORM, LOW REYNOLDS NUMBER, LOW ADVANCE RATIO
 
 
References: 
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Citations: 
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+ Click to Cite.
APA: Copy

LIU, Z., & LIU, P., & QU, Q., & HU, T. (2016). EFFECT OF ADVANCE RATIO AND BLADE PLANFORM ON THE PROPELLER PERFORMANCE OF A HIGH ALTITUDE AIRSHIP. JOURNAL OF APPLIED FLUID MECHANICS (JAFM), 9(6), 2993-3000. https://www.sid.ir/en/journal/ViewPaper.aspx?id=573255



Vancouver: Copy

LIU Z., LIU P., QU Q., HU T.. EFFECT OF ADVANCE RATIO AND BLADE PLANFORM ON THE PROPELLER PERFORMANCE OF A HIGH ALTITUDE AIRSHIP. JOURNAL OF APPLIED FLUID MECHANICS (JAFM). 2016 [cited 2021July29];9(6):2993-3000. Available from: https://www.sid.ir/en/journal/ViewPaper.aspx?id=573255



IEEE: Copy

LIU, Z., LIU, P., QU, Q., HU, T., 2016. EFFECT OF ADVANCE RATIO AND BLADE PLANFORM ON THE PROPELLER PERFORMANCE OF A HIGH ALTITUDE AIRSHIP. JOURNAL OF APPLIED FLUID MECHANICS (JAFM), [online] 9(6), pp.2993-3000. Available: https://www.sid.ir/en/journal/ViewPaper.aspx?id=573255.



 
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