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New Results in Numerical and Experimental Fluid Mechanics XIII = Contributions to the 22nd STAB/DGLR Symposium /
紀錄類型:
書目-語言資料,印刷品 : Monograph/item
正題名/作者:
New Results in Numerical and Experimental Fluid Mechanics XIII/ edited by Andreas Dillmann, Gerd Heller, Ewald Krämer, Claus Wagner.
其他題名:
Contributions to the 22nd STAB/DGLR Symposium /
其他作者:
Wagner, Claus.
面頁冊數:
XIV, 787 p. 512 illus., 431 illus. in color.online resource. :
Contained By:
Springer Nature eBook
標題:
Classical and Continuum Physics. -
電子資源:
https://doi.org/10.1007/978-3-030-79561-0
ISBN:
9783030795610
New Results in Numerical and Experimental Fluid Mechanics XIII = Contributions to the 22nd STAB/DGLR Symposium /
New Results in Numerical and Experimental Fluid Mechanics XIII
Contributions to the 22nd STAB/DGLR Symposium /[electronic resource] :edited by Andreas Dillmann, Gerd Heller, Ewald Krämer, Claus Wagner. - 1st ed. 2021. - XIV, 787 p. 512 illus., 431 illus. in color.online resource. - Notes on Numerical Fluid Mechanics and Multidisciplinary Design,1511612-2909 ;. - Notes on Numerical Fluid Mechanics and Multidisciplinary Design,126.
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.
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. .
ISBN: 9783030795610
Standard No.: 10.1007/978-3-030-79561-0doiSubjects--Topical Terms:
1141497
Classical and Continuum Physics.
LC Class. No.: TA357-359
Dewey Class. No.: 620.1064
New Results in Numerical and Experimental Fluid Mechanics XIII = Contributions to the 22nd STAB/DGLR Symposium /
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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.
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