A 1-DOF Wind Tunnel Experiment in Adaptive Flow Control

Author(s):  
Ali Kutay ◽  
Anthony Calise ◽  
Jonathan Muse
2022 ◽  
Author(s):  
Case P. Van Dam ◽  
Sai B. Mothukuri ◽  
Seyedeh Sheida Hosseini ◽  
Edward White ◽  
Lisa Brown ◽  
...  

2018 ◽  
Vol 65 (8) ◽  
pp. 1049-1062 ◽  
Author(s):  
Zanyar Feizi ◽  
Shamsollah Ayoubi ◽  
Mohammad Reza Mosaddeghi ◽  
Ali Asghar Besalatpour ◽  
Mojtaba Zeraatpisheh ◽  
...  

2014 ◽  
Vol 716-717 ◽  
pp. 764-766
Author(s):  
Min Jiang ◽  
Ji He Zhou

On the basis of javelin wind tunnel experiment, we established mathematical model of javelin flight to conduct a computer optimization and got the conclusions. When the initial velocity is in the range of 25m/s-30m/s, the best throwing condition is: the throwing angle is 40°, the angle of attack is 11°. The javelin throwing condition is not zero angle of attack was necessary and sufficient for obtained aerodynamic efficiency.


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