Nomograms for determining sonic-boom overpressure.
Nomograms for rapid calculation of maximum ground sonic-boom overpressure for different flight conditions
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Effects of temporal tangential bearing acceleration on performance characteristics of slider and journal bearings
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Nomogram for correcting drag and angle of attack of an airfoil model in an air stream of finite diameter
In experimenting with airfoil models in a wind tunnel, the magnitude of the forces acting on the model is affected by the fact that the air stream in which the model is suspended, has a restricted cross-section. In order to utilize the results for an airplane in an unlimited quantity of air, a correction must be made. The magnitude of this correction was determined by Prandtl by the application of his wing theory.
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