Panel code estimates of wind tunnel wall and support interference effects on the HSCT

2000 ◽  
Author(s):  
Robert Griffiths ◽  
Kenneth Visser
Keyword(s):  
Wind Tunnel ◽  
Interference Effects ◽  
Tunnel Wall ◽  
Support Interference

Wind-Tunnel Wall Interference Effects on a Supercritical Airfoil at Transonic Speeds

1977 ◽  
Vol 14 (10) ◽  
pp. 929-935 ◽  
Author(s):  
James A. Blackwell ◽  
Gerald A. Pounds
Keyword(s):  
Wind Tunnel ◽  
Interference Effects ◽  
Tunnel Wall ◽  
Supercritical Airfoil

Wind-Tunnel Wall Interference Effects for 20° Cone-Cylinders

1973 ◽  
Vol 10 (10) ◽  
pp. 671-678 ◽  
Author(s):  
JOHN WILLIAM DAVIS ◽  
ROBERT F. GRAHAM
Keyword(s):  
Wind Tunnel ◽  
Interference Effects ◽  
Tunnel Wall

Analysis of Wind Tunnel Wall Interference Effects on Subsonic Unsteady Airfoil Flows

2007 ◽  
Vol 44 (5) ◽  
pp. 1683-1690 ◽  
Author(s):  
Karthikeyan Duraisamy ◽  
William J. McCroskey ◽  
James D. Baeder
Keyword(s):  
Wind Tunnel ◽  
Interference Effects ◽  
Tunnel Wall

Transonic airfoil calculations including wind tunnel wall-interference effects

AIAA Journal ◽  
1986 ◽  
Vol 24 (8) ◽  
pp. 1378-1380 ◽  
Author(s):  
L. S. King ◽  
D. A. Johnson
Keyword(s):  
Wind Tunnel ◽  
Interference Effects ◽  
Tunnel Wall ◽  
Transonic Airfoil

scholarly journals Cable Suspension and Balance System with Low Support Interference and Vibration for Effective Wind Tunnel Tests

2021 ◽  
Author(s):  
Keum-Yong Park ◽  
Yeol-Hun Sung ◽  
Jae-Hung Han
Keyword(s):  
Wind Tunnel ◽  
Vibration Suppression ◽  
Aerodynamic Load ◽  
Test Model ◽  
Wind Tunnel Tests ◽  
Balance System ◽  
Motion Responses ◽  
Vibration Responses ◽  
Aerodynamic Interference ◽  
Support Interference

AbstractA cable-driven model support concept is suggested and implemented in this paper. In this case, it is a cable suspension and balance system (CSBS), which has the advantages of low support interference and reduced vibration responses for effective wind tunnel tests. This system is designed for both model motion control and aerodynamic load measurements. In the CSBS, the required position or the attitude of the test model is realized by eight motors, which adjust the length, velocity, and acceleration of the corresponding cables. Aerodynamic load measurements are accomplished by a cable balance consisting of eight load cells connected to the assigned cables. The motion responses and load measurement outputs were in good agreement with the reference data. The effectiveness of the CSBS against aerodynamic interference and vibration is experimentally demonstrated through comparative tests with a rear sting and a crescent sting support (CSS). The advantages of the CSBS are examined through several wind tunnel tests of a NACA0015 airfoil model. The cable support of the CSBS clearly showed less aerodynamic interference than the rear sting with a CSS, judging from the drag coefficient profile. Additionally, the CSBS showed excellent vibration suppression characteristics at all angles of attack.

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