THE present edition is enlarged to provide, in the first place, an introduction to the mathematical and experimental study of compressible flow, subsonic and supersonic. This and other matters now becoming prominent are not collected in a supplementary section but incorporated in place as additional articles or short chapters. Following a well-established practice, the numbering of original articles, figures and chapters is left undisturbed as far as possible, interpolations being distinguished by letter-suffixes. It is hoped this procedure will ensure a minimum of inconvenience to readers familiar with the earlier edition. To some extent the unlettered articles indicate a first course of reading, though a modern view of Aerodynamics requires consideration of Mach numbers equally with Reynolds numbers almost from the outset.
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Labels: Physics