Influence of Transonic Flow on the Thrust Determination of TPS during Wind Tunnel measurements
Geyr, H. von and Rossow, C.-C. and Hoheisel, H. (2004) Influence of Transonic Flow on the Thrust Determination of TPS during Wind Tunnel measurements. In: New Results in Numerical and Experimental Fluid Mechanics IV, 87, pp. 475-482. Springer Verlag, Berlin, Heidelberg, New York. 13th STAB/DGLR Symposium, München (de), 12.-14.11.2002. ISBN 3-540-20258-7.
Full text not available from this repository.
The drag determination of powered configurations equipped with Turbine-Powered-Simulators (TPS) at transonic speeds in the wind tunnel is basically the problem of correct net thrust determination, since neither drag nor thrust can be measured directly. For thrust evaluation the Standard-Bookkeeping-Method (SBM) is applied, which computes the gross thrust from measured quantities and coefficients, which are obtained during static engine calibration. In wind tunnel experiments, peculiar drag behaviour was observed in terms of the effect of power settings and the influence of different bypass ratios (BPR). Within this contribution analysis using CFD are performed to demonstrate the influence of external flow on the gross thrust for an isolated TPS. From the obtained results the shortcomings of the SBM at transonic external flow are identified and a thrust corrections to the derived. The application of the corrections to the measured Lilienthal-polars stress the necessity of a valid bookkeeping procedure for transonic Mach numbers.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||Influence of Transonic Flow on the Thrust Determination of TPS during Wind Tunnel measurements|
|Journal or Publication Title:||New Results in Numerical and Experimental Fluid Mechanics IV|
|Page Range:||pp. 475-482|
|Publisher:||Springer Verlag, Berlin, Heidelberg, New York|
|Series Name:||Notes on Numerical Fluid Mechanics and Multidisciplinary Design|
|Keywords:||TPS thrust determination, CFD, thrust-drag bookkeeping|
|Event Title:||13th STAB/DGLR Symposium, München (de), 12.-14.11.2002|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L AR - Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||L - Concepts & Integration|
|Location:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||31 Jan 2006|
|Last Modified:||14 Jan 2010 19:27|
Repository Staff Only: item control page