The application of the pressure sensitive paint technique to high speed wind tunnel testing of a fighter aircraft configuration with complex store loadings

1994 ◽  
Author(s):  
Robert Dowgwillo ◽  
Martin Morris ◽  
John Donovan ◽  
Michael Benne
Keyword(s):  
Wind Tunnel ◽  
High Speed ◽  
Wind Tunnel Testing ◽  
Pressure Sensitive Paint ◽  
Fighter Aircraft ◽  
Pressure Sensitive ◽  
Tunnel Testing

Pressure sensitive paint in transonic wind-tunnel testing of the F-15

1996 ◽  
Vol 33 (1) ◽  
pp. 109-116 ◽  
Author(s):  
Robert M. Dowgwillo ◽  
Martin J. Morris ◽  
John F. Donovan ◽  
Michael E. Benne
Keyword(s):  
Wind Tunnel ◽  
Wind Tunnel Testing ◽  
Pressure Sensitive Paint ◽  
Pressure Sensitive ◽  
Transonic Wind Tunnel ◽  
Tunnel Testing

Novel pressure-sensitive paint for cryogenic and unsteady wind tunnel testing

2000 ◽  
Author(s):  
Keisuke Asai ◽  
Yutaka Amao ◽  
Yoshimi Iijima ◽  
Ichiro Okura ◽  
Hiroyuki Nishide
Keyword(s):  
Wind Tunnel ◽  
Wind Tunnel Testing ◽  
Pressure Sensitive Paint ◽  
Pressure Sensitive ◽  
Tunnel Testing

Temperature Correction of Pressure-Sensitive Paint for Industrial Wind Tunnel Testing

2006 ◽  
Vol 43 (5) ◽  
pp. 1499-1505 ◽  
Author(s):  
Mitsuru Kurita ◽  
Kazuyuki Nakakita ◽  
Kazunori Mitsuo ◽  
Shigeya Watanabe
Keyword(s):  
Wind Tunnel ◽  
Temperature Correction ◽  
Wind Tunnel Testing ◽  
Pressure Sensitive Paint ◽  
Pressure Sensitive ◽  
Tunnel Testing

Novel Pressure-Sensitive Paint for Cryogenic and Unsteady Wind-Tunnel Testing

2002 ◽  
Vol 16 (1) ◽  
pp. 109-115 ◽  
Author(s):  
Keisuke Asai ◽  
Yutaka Amao ◽  
Yoshimi Iijima ◽  
Ichiro Okura ◽  
Hiroyuki Nishide
Keyword(s):  
Wind Tunnel ◽  
Wind Tunnel Testing ◽  
Pressure Sensitive Paint ◽  
Pressure Sensitive ◽  
Tunnel Testing

Videogrammetry of the Model’s Attitude in Wind Tunnel Testing

2012 ◽  
Vol 190-191 ◽  
pp. 1273-1277 ◽  
Author(s):  
Zheng Yu Zhang ◽  
Zhong Xiang Sun ◽  
Xu Hui Huang ◽  
Yan Sun
Keyword(s):  
Standard Deviation ◽  
Wind Tunnel ◽  
Drag Coefficient ◽  
Systematic Error ◽  
Measurement System ◽  
High Speed ◽  
Wind Tunnel Test ◽  
Wind Tunnel Testing ◽  
Supersonic Wind Tunnel ◽  
Tunnel Testing

The advanced precision of drag coefficient is 0.0001 for the high speed wind tunnel test of measuring forces, the model’s angle of attack precision is ≤0.01°following errors distribution. A videogrammetric method of model’s attitude is therefore proposed, its uncertainty is investigated, and a compensation method of its systematic error is also presented by this paper. The three engineering videogrammetric experiments of attack angle in 2 meter supersonic wind tunnel testing have demonstrated that measuring standard deviation of videogrammetric measurement system established by this paper is ≤0.0094°, in addition it neither destroys the model’s shape, nor changes the stiffness or strength, so it is useful and effective.

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