Dillmann / Heller / Krämer New Results in Numerical and Experimental Fluid Mechanics XIII

Contributions to the 22nd STAB/DGLR Symposium
1. Auflage 2021
ISBN: 978-3-030-79561-0
Verlag: Springer International Publishing
Format: PDF
Kopierschutz: 1 - PDF Watermark

E-Book, Englisch, Band 151, 787 Seiten, eBook

Reihe: Notes on Numerical Fluid Mechanics and Multidisciplinary Design

This book offers timely insights into research on numerical and experimental fluid mechanics and aerodynamics, mainly for (but not limited to) aerospace applications. It reports on findings by members of the STAB (German Aerospace Aerodynamics Association) and DGLR (German Society for Aeronautics and Astronautics) and covers both nationally and EC-funded projects. Continuing on the tradition of the previous volumes, the book highlights innovative solutions, promoting translation from fundamental research to industrial applications. It addresses academics and professionals in the field of aeronautics, astronautics, ground transportation, and energy alike.

Zielgruppe

Research

Autoren/Hrsg.

Dillmann, Andreas

Heller, Gerd

Krämer, Ewald

Wagner, Claus

Inhaltsverzeichnis

Influence of the Wind Tunnel Model Mounting on the Wake Evolution of the Common Research Model in Post Stall.- Assessment of the Disturbance Velocity Approach to Determine the Gust Impact on Airfoils in Transonic Flow.- Comparison of Different Methods for the Extraction of Airfoil Characteristics of Propeller Blades as Input for Propeller Models in CFD.- Stochastic Modeling of Passive Scalars in Turbulent Channel Flows: Predictive Capabilities of One-Dimensional Turbulence.- Study on Large-Scale Amplitude Modulation of Near-Wall Small-Scale Structures in Turbulent Wall-Bounded Flows.- Investigation of Coherent Motions in a Flat-Plate Turbulent Boundary Layer with Adverse Pressure Gradient.- Experimental Approach on Concentration Measurements of NO in Hydrogen Combustion based on Heterodyne Laser Absorption Spectroscopy using Quantum Cascade Lasers.- Internal Application of Ultra-Fast Temperature Sensitive Paint to Hydrogen Combustion Flow.- Influence of Surface Irregularities on the Expected Boundary-Layer Transition Location on Hybrid Laminar Flow Control Wings.