Six-DoF UAV simulation using wind tunnel test data and its cruise mode autopilot design

2014 ◽  
Author(s):  
Kalpit S. Mehta ◽  
Kamlesh Kumar ◽  
R B Jagadeeshchandra
Keyword(s):  
Wind Tunnel ◽  
Test Data ◽  
Wind Tunnel Test ◽  
Six Dof

Blockage effect correction for a scaled wind turbine rotor by using wind tunnel test data

2015 ◽  
Vol 79 ◽  
pp. 227-235 ◽  
Author(s):  
Jaeha Ryi ◽  
Wook Rhee ◽  
Ui Chang Hwang ◽  
Jong-Soo Choi
Keyword(s):  
Wind Tunnel ◽  
Wind Turbine ◽  
Test Data ◽  
Wind Tunnel Test ◽  
Turbine Rotor ◽  
Wind Turbine Rotor ◽  
Blockage Effect

scholarly journals Numerical CFD Simulation and Test Correlation in a Flight Project Environment

2015 ◽  
Author(s):  
K. K. Gupta ◽  
S. F. Lung ◽  
A. H. Ibrahim
Keyword(s):  
Wind Tunnel ◽  
Test Data ◽  
Cfd Simulation ◽  
Wind Tunnel Test ◽  
Flight Testing ◽  
Project Environment ◽  
Test Correlation

This paper presents detailed description of a novel CFD procedure and comparison of its solution results to that obtained by other available CFD codes as well as actual flight and wind tunnel test data pertaining to the GIII aircraft, currently undergoing flight testing at AFRC.

Design and Application of an all Moving Wing Model Limiting and Locking Device

2013 ◽  
Vol 753-755 ◽  
pp. 1031-1034 ◽  
Author(s):  
Bo Lu ◽  
Bin Bin Lv ◽  
Li Yu ◽  
Hong Tao Guo ◽  
Yu Yan ◽  
...  
Keyword(s):  
Wind Tunnel ◽  
Test Data ◽  
High Speed ◽  
Wind Tunnel Test ◽  
Test Equipment ◽  
Test Model ◽  
Wing Flutter ◽  
Wing Model ◽  
Control Principle ◽  
Design And Application

To effectively excite the all moving wing flutter model and limiting or quick locking model in case of bigger amplitude of the model, an excitation and limiting and locking device is designed for the high-speed wind tunnel flutter test model. This paper introduces the structure arrangement, control principle and strategy of this device. The wind tunnel flutter test indicates that this device can enhance the SNR of the test data, improve the boundary prediction precision of flutter, prevent the model from entering the flutter divergence state and protect the model and wind tunnel test equipment.

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