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Excerpt from Detatched-Shock Calculations by Power Series, I The stand-off distance is of the order of one tenth the radius of curvature of the body at the nose, the actual distance depending on the mach number and the assumed equation of state. Near the axis, the flow is subsonic; farther away it is supersonic. Under usual conditions, the boundary layer that builds up adjacent to the body is of negligible thickness; therefore, the assumption of an inviscid flow throughout most of the interesting region is Justified. About the Publisher Forgotten Books publishes hundreds of thousands of rare and classic books. Find more at www.forgottenbooks.com This book is a reproduction of an important historical work. Forgotten Books uses state-of-the-art technology to digitally reconstruct the work, preserving the original format whilst repairing imperfections present in the aged copy. In rare cases, an imperfection in the original, such as a blemish or missing page, may be replicated in our edition. We do, however, repair the vast majority of imperfections successfully; any imperfections that remain are intentionally left to preserve the state of such historical works.

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