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Force and Pressure Tests of an Agard Calibration Model B at a Mach Number of 10

Report Number: AEDC TDR 64-31
Author(s): R. K. Matthews and L. L. Trimmer
Corporate Author: ARO, Inc.
Date of Publication: 1964-02
Pages: 28
Contract: AF 40(600)-1000
Project: None Given
AD Number: AD0430701

Abstract:
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.

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