Abstract:Solutions for point and line sources are given, for the `transient ’ case only, in both stationary and moving co-ordinate systems. These are then integrated to give the solutions for a supersonic aerofoil (
a
) entering a sharp-edged gust, (
b
)following a sudden change of incidence. The method of obtaining oscillatory (flutter) solutions from (
b
) comes next, and it is Finally, the results of some calculations on the entry of supersonic … Show more
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