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T - Technology
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Boundary layer

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1.
Flight-measured base pressure coefficients for thick boundary-layer flow over an aft-facing step for Mach numbers from 0.4 to 2.5
Author
Goecke, Sheryll A.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973.
Location
Library Shelving Facility (LSF) >> NASA TN D-7202
Format
Books