scholarly journals An overview of X-38 hypersonic aerothermodynamic wind tunnel data and comparison with numerical results

1997 ◽  
Author(s):  
Charles Campbell ◽  
Jose Caram ◽  
Scott Berry ◽  
Thomas Horvath ◽  
N. Merski ◽  
...  
Keyword(s):  
Wind Tunnel ◽  
Numerical Results ◽  
Wind Tunnel Data

scholarly journals An overview of X-38 Hypersonic Wind Tunnel data and comparison with numerical results

1997 ◽  
Author(s):  
Charles Campbell ◽  
Jose Caram ◽  
Scott Berry ◽  
Michael DiFulvio ◽  
Tom Horvath ◽  
...  
Keyword(s):  
Wind Tunnel ◽  
Numerical Results ◽  
Hypersonic Wind Tunnel ◽  
Wind Tunnel Data

Comparison of free-flight and wind tunnel data for a generic fighterconfiguration

1982 ◽  
Author(s):  
G. WINCHENBACH ◽  
R. CHELEKIS ◽  
B. USELTON ◽  
W. HATHAWAY
Keyword(s):  
Wind Tunnel ◽  
Free Flight ◽  
Wind Tunnel Data

A comparison of mesh-adaptive LES with wind tunnel data for flow past buildings: Mean flows and velocity fluctuations

2009 ◽  
Vol 43 (39) ◽  
pp. 6238-6253 ◽  
Author(s):  
Elsa Aristodemou ◽  
Tom Bentham ◽  
Christopher Pain ◽  
Roy Colvile ◽  
Alan Robins ◽  
...  
Keyword(s):  
Wind Tunnel ◽  
Velocity Fluctuations ◽  
Flow Past ◽  
Wind Tunnel Data

On-Road Aerodynamic Drag Measurements Compared with Wind Tunnel Data

1995 ◽  
Author(s):  
G. M. Le Good ◽  
J. P. Howell ◽  
M. A. Passmore ◽  
K. P. Garry
Keyword(s):  
Wind Tunnel ◽  
Aerodynamic Drag ◽  
Wind Tunnel Data

An application of automatic carpet plotting to wind-tunnel data reduction.

1967 ◽  
Vol 4 (3) ◽  
pp. 408-410 ◽  
Author(s):  
DENNIS M. JECMEN ◽  
J. PETER REDING ◽  
LARS E. ERICSSON
Keyword(s):  
Wind Tunnel ◽  
Data Reduction ◽  
Wind Tunnel Data

Surface Pressure Distribution on a Blade of a 10 m Diameter HAWT (Field Measurements versus Wind Tunnel Measurements)

2005 ◽  
Vol 127 (2) ◽  
pp. 185-191 ◽  
Author(s):  
T. Maeda ◽  
E. Ismaili ◽  
H. Kawabuchi ◽  
Y. Kamada
Keyword(s):  
Wind Tunnel ◽  
Surface Pressure ◽  
Field Measurements ◽  
Reynolds Numbers ◽  
Blade Surface ◽  
Pressure Data ◽  
Surface Pressure Distribution ◽  
Pressure Distributions ◽  
Wind Tunnel Data ◽  
Local Angle

This paper exploits blade surface pressure data acquired by testing a three-bladed upwind turbine operating in the field. Data were collected for a rotor blade at spanwise 0.7R with the rotor disc at zero yaw. Then, for the same blade, surface pressure data were acquired by testing in a wind tunnel. Analyses compared aerodynamic forces and surface pressure distributions under field conditions against analogous baseline data acquired from the wind tunnel data. The results show that aerodynamic performance of the section 70%, for local angle of attack below static stall, is similar for free stream and wind tunnel conditions and resemblances those commonly observed on two-dimensional aerofoils near stall. For post-stall flow, it is presumed that the exhibited differences are attributes of the differences on the Reynolds numbers at which the experiments were conducted.

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