14   Artículos

 
en línea
Shuai Ma, Jun Hu, Xuegao Wang and Jiajia Ji    
To make measurement of end-wall flow between blade rows in a compact multistage configuration possible, a miniature L-shaped five-hole probe was employed in this paper. This compact tip structure, realized by laser-printing instead of the conventional ma... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Loris Simonassi, Gustavo Lopes and Sergio Lavagnoli    
The influence of unsteady wakes incoming from the upstream stages is of high relevance in modern high-speed, low-pressure turbines (LPT) operating at transonic exit Mach numbers and low Reynolds numbers for their potential to trigger transition and influ... ver más

 
en línea
Reinaldo A. Gomes, Julia Kurz and Reinhard Niehuis    
Flow measurement using a linear compressor or turbine cascade is a well-established technique to characterize the flow in turbomachines with a certain degree of abstraction. A common way to obtain a general characterization of the flow is to measure the ... ver más

 
en línea
Hermann Knaus, Martin Hofsäß, Alexander Rautenberg and Jens Bange    
A model for the simulation of wind flow in complex terrain is presented based on the Reynolds averaged Navier?Stokes (RANS) equations. For the description of turbulence, the standard k-e, the renormalization group (RNG) k-e, and a Reynolds stress turbule... ver más
Revista: Computation    Formato: Electrónico

 
en línea
Brandon M. Witte, Robert F. Singler and Sean C. C. Bailey    
This paper describes the components and usage of an unmanned aerial vehicle developed for measuring turbulence in the atmospheric boundary layer. A method of computing the time-dependent wind speed from a moving velocity sensor data is provided. The phys... ver más
Revista: Atmosphere    Formato: Electrónico

 
en línea
Florian Knoth and Christian Breitsamter    
Aerodynamic characteristics of helicopter engine side air intakes are investigated. The experimental data set is obtained by wind tunnel testing of a full-scale helicopter fuselage section model. For the simulation of realistic engine operation, engine m... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Holger Werschnik, Marius Schneider, Janina Herrmann, Dimitri Ivanov, Heinz-Peter Schiffer and Christoph Lyko    
The aerothermal interaction of the combustor exit flow on the first vane row has been examined at the Large Scale Turbine Rig (LSTR) at Technische Universität Darmstadt (Darmstadt, Germany). A baseline configuration of axial inflow and a variation of swi... ver más

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