The Numerical Analysis and Experimental Study of Flux Switching Motor/Generator in HEV Applications

2016 ◽  
Vol 52 (15) ◽  
pp. 100 ◽  
Author(s):  
Minchao CUI
Keyword(s):  
Experimental Study ◽  
Numerical Analysis ◽  
Flux Switching Motor

Numerical analysis and experimental study of an ocean wave tetrahedral triboelectric nanogenerator

2021 ◽  
pp. 118174
Author(s):  
Anqun Wang ◽  
Jun Chen ◽  
Li Wang ◽  
Junlei Han ◽  
Weiguang Su ◽  
...  
Keyword(s):  
Experimental Study ◽  
Numerical Analysis ◽  
Ocean Wave ◽  
Triboelectric Nanogenerator

Numerical analysis and experimental study of the magnetic lifting device prototype

2015 ◽  
Vol 27 (7) ◽  
pp. 76003
Author(s):  
赵丽霞 Zhao Lixia ◽  
吕明邦 Lü Mingbang ◽  
张翔 Zhang Xiang ◽  
于海燕 Yu Haiyan ◽  
姚庆高 Yao Qinggao ◽  
...  
Keyword(s):  
Experimental Study ◽  
Numerical Analysis

Experimental Study of Graphite Ablation in Nitrogen Flow, Part II: Further Numerical Analysis

2010 ◽  
Vol 24 (3) ◽  
pp. 589-597 ◽  
Author(s):  
Toshiyuki Suzuki ◽  
Kazuhisa Fujita ◽  
Takeharu Sakai
Keyword(s):  
Experimental Study ◽  
Numerical Analysis ◽  
Nitrogen Flow ◽  
Flow Part

scholarly journals Experimental Study of Aircraft Achieving Dutch Roll Mode Stability without Weathercock Stability

2020 ◽  
Vol 2020 ◽  
pp. 1-8
Author(s):  
Jingcheng Fu ◽  
Jun Huang ◽  
Lei Song ◽  
Daqing Yang
Keyword(s):  
Experimental Study ◽  
Numerical Analysis ◽  
Quality Analysis ◽  
Flight Experiment ◽  
Handling Characteristics ◽  
Marginal Change ◽  
Mode Stability ◽  
Mode Characteristics ◽  
The Difference ◽  
Dutch Roll

Weathercock stability is usually considered essential to achieve normal flight, while the Dutch roll mode stability can still be achieved without weathercock stability which has been algebraically proved. This paper proposed a flight experiment to investigate the characteristics of an airplane with Dutch roll mode stability but no weathercock stability. Firstly, the algebraic analysis based on a standard lateral-directional mode approximation was made to demonstrate the effect of yawing stability derivative Cnβ on the Dutch roll mode characteristics. The flight experiment was organized after that using a model glider which was modified to have zero Cnβ but with marginal change on Cyβ. The convergence of Dutch roll mode in flight meets the algebraic and numerical analysis as expected. However, the difference of handling characteristics between the original and modified configurations indicates some other roles the weathercock stability plays in flight as well as some limitations of utilizing mode criterion in flight quality analysis.

Numerical Analysis and Experimental Study on Magnetic Fluid Reciprocating Seals

2019 ◽  
Vol 55 (1) ◽  
pp. 1-6 ◽  
Author(s):  
Yibiao Chen ◽  
Decai Li ◽  
Yanjuan Zhang ◽  
Chunyan He
Keyword(s):  
Experimental Study ◽  
Numerical Analysis ◽  
Magnetic Fluid
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