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Force and Pressure Tests of an AGARD Calibration Model B at a Mach Number of 10
Richard K. Matthews
L. L. Trimmer
出版
Arnold Engineering Development Center, Air Force Systems Command, United States Air Force
, 1964
URL
http://books.google.com.hk/books?id=nnwYVwctPtEC&hl=&source=gbs_api
註釋
The AGARD Calibration Model B, with and without wings, was tested at a nominal Mach number of 10. Force and moment coefficients were obtained over a range of pitch and yaw angles from -5 to 15.5 degrees with a Reynolds number range from 1.10 x 10 to the 6th power to 9.80 x 10 to the 6th power, based on model length. The lift-curve slope, aerodynamic center, and drag coefficients show excellent correlation with data from other tunnels at various Mach numbers. (Author).
