Titlebook: New Results in Numerical and Experimental Fluid Mechanics II; Contributions to the Wolfgang Nitsche,Hans-Joachim Heinemann,Reinhard H Book

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In-flight Boundary Layer Investigations on a Laminar Wing using Laser Doppler Anemometry,presented. In order to characterise the development of the Tollmien-Schlichting wave spectral and harmonic analysis were adopted. Finally, suggestions for further advancements of the LDA systems are proposed.

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Strake Effects On the Turbulent Fin Flowfield Of a High-Performance Fighter Aircraft,r for the strake-on compared to the strake-off configuration. Moreover, the observed narrow-band concentration of turbulent kinetic energy is also less severe that the excitation level on fin structural modes is reduced.

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