Experimental Measurements in the Turbulent Boundary Layer of a Yawed, Spinning Ogive-Cylinder Body of Revolution at Mach 3.0. Part 2. Data Tabulation
ARMY BALLISTIC RESEARCH LAB ABERDEEN PROVING GROUND MD
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This report presents a tabulation of data for the experiment which is fully described in Part I. Experiment and Data Analysis. The data consist of turbulent boundary layer profile characteristics and wall shear stress for a yawed, spinning slender body of revolution at Mach 3 for angles of attack up to 6.3 degrees. The data tabulations are presented in a format which facilitates their use for comparison to theoretical computations.
- Fluid Mechanics