Theoretical Pressure Distributions On Wings Of Finite Span At Zero Incidence For Mach Numbers Near 1
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Theoretical Pressure Distributions on Wings of Finite Span at Zero Incidence for Mach Numbers Near 1
Author | : Alberta Y. Alksne |
Publisher | : |
Total Pages | : 56 |
Release | : 1961 |
Genre | : Aerodynamics, Transonic |
ISBN | : |
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The first Symposium Transsonicum took pl.ace in Aachen thirteen years ago during a period of decreasing governmental. and industrial. support for transonic flow