Low-speed wind tunnel test results of the Canard Rotor/Wing concept

1993 ◽  
Author(s):  
STEVEN BASS ◽  
THOMAS THOMPSON ◽  
JOHN RUTHERFORD ◽  
STEPHEN SWANSON
Keyword(s):  
Wind Tunnel ◽  
Wind Tunnel Test ◽  
Test Results ◽  
Low Speed ◽  
Rotor Wing ◽  
Low Speed Wind Tunnel

LOW SPEED WIND TUNNEL TEST OF THE JET TRAINER MODEL AT HIGH ANGLES OF ATTACK

2016 ◽  
Vol 23 (4) ◽  
pp. 471-478
Author(s):  
Kamil Smędra ◽  
Rafał Świerkot ◽  
Krzysztof Kubryński
Keyword(s):  
Wind Tunnel ◽  
Wind Tunnel Test ◽  
Low Speed ◽  
Low Speed Wind Tunnel ◽  
High Angles Of Attack

scholarly journals High lift device design and low speed wind-tunnel test.

1986 ◽  
Vol 34 (394) ◽  
pp. 592-599
Author(s):  
Masanobu OGAKI ◽  
Takeshi WATANABE ◽  
Kanichi AMANO
Keyword(s):  
Wind Tunnel ◽  
Wind Tunnel Test ◽  
Device Design ◽  
High Lift ◽  
Low Speed ◽  
Low Speed Wind Tunnel

Effects of Aircraft Tail Configurations on Sensitivity to Yaw Disturbances

2014 ◽  
Vol 629 ◽  
pp. 197-201 ◽  
Author(s):  
Nur Amalina Musa ◽  
S. Mansor ◽  
Airi Ali ◽  
Wan Zaidi Wan Omar ◽  
Ainullotfi Abdul Latif ◽  
...  
Keyword(s):  
Wind Tunnel ◽  
Wind Tunnel Test ◽  
Aerodynamic Characteristics ◽  
Low Speed ◽  
Stability And Control ◽  
Directional Stability ◽  
And Control ◽  
Low Speed Wind Tunnel ◽  
Yaw Moment ◽  
Made In

A wind tunnel test was conducted to compare the characteristics of low speed stability and control for aircraft with conventional tail and V-tail configurations. Comparison was made in terms of static directional stability at selected test speed of 40 m/s, which corresponds to Reynolds number of 0.1622 x 106 based on the chord. Three types of simplified tail-only model were tested in Universiti Teknologi Malaysia's Low Speed Wind Tunnel (UTM-LST). Results show that the V-tail configuration greatly affects the aerodynamic characteristics in directional stability as the side force and yaw moment tends to vary linearly with yaw angles up to 25 degrees, compared to conventional tail that has linear characteristics up to only 10 degrees yaw

Sign in / Sign up

Export Citation Format

Share Document