Experimental and analytical investigation of contra-rotating multi-rotor UAV propeller noise

2021 ◽  
Vol 177 ◽  
pp. 107850
Author(s):  
Ryan S. McKay ◽  
Michael J. Kingan ◽  
Sung Tyaek Go ◽  
Riul Jung
Planta Medica ◽  
2012 ◽  
Vol 78 (05) ◽  
Author(s):  
M Wang ◽  
A Chittiboyina ◽  
B Avula ◽  
J Zhao ◽  
N Tabanca ◽  
...  

2021 ◽  
Vol 63 ◽  
pp. 102484
Author(s):  
Luís C.B. Silva ◽  
Carlos E.S. Castellani ◽  
Marcelo E.V. Segatto ◽  
Maria J. Pontes

Author(s):  
Samuel Tilahun ◽  
Velmurugan Paramasivam ◽  
Mebratu Tufa ◽  
Alelign kerebih ◽  
Senthil Kumaran Selvaraj

2021 ◽  
Author(s):  
Mazin Tahir ◽  
Amirmohammad Rahimizadeh ◽  
Jordan Kalman ◽  
Kazem Fayazbakhsh ◽  
Larry Lessard

CivilEng ◽  
2021 ◽  
Vol 2 (2) ◽  
pp. 442-458
Author(s):  
Sandip Chhetri ◽  
Rachel A. Chicchi

Experimental testing of deformed rebar anchors (DRAs) has not been performed extensively, so there is limited test data to understand their failure behavior. This study aims to expand upon these limited tests and understand the behavior of these anchors, when loaded in tension. Analytical benchmark models were created using available test data and a parametric study of deformed rebar anchors was performed. Anchor diameter, spacing, embedment, and number of anchors were varied for a total of 49 concrete breakout simulations. The different failure modes of anchors were predicted analytically, which showed that concrete breakout failure is prominent in the DRA groups. The predicted concrete breakout values were consistent with mean and 5% fractile concrete capacities determined from the ACI concrete capacity design (CCD) method. The 5% fractile factor determined empirically from the simulation results was kc = 26. This value corresponds closely with kc = 24 specified in ACI 318-19 and ACI 349-13 for cast-in place anchors. The analysis results show that the ACI CCD formula can be conservatively used to design DRAs loaded in tension by applying a kc factor no greater than 26.


Author(s):  
M. Zugic ◽  
J. R. Culham ◽  
P. Teertstra ◽  
Y. Muzychka ◽  
K. Horne ◽  
...  

Compact, liquid cooled heat sinks are used in applications where high heat fluxes and boundary resistance preclude the use of more traditional air cooling techniques. Four different liquid cooled heat sink designs, whose core geometry is formed by overlapped ribbed plates, are examined. The objective of this analysis is to develop models that can be used as design tools for the prediction of overall heat transfer and pressure drop of heat sinks. Models are validated for Reynolds numbers between 300 and 5000 using experimental tests. The agreement between the experiments and the models ranges from 2.35% to 15.3% RMS.


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