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Influence of transonic Flow on the Thrust Determination of TPS during Wind Tunnel measurements

Geyr, H. von and Rossow, C.-C. and Hoheisel, H. (2002) Influence of transonic Flow on the Thrust Determination of TPS during Wind Tunnel measurements. 13. DGLR-Fachsymposium der AG STAB, München (de), 12.-14.11.2002.

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Abstract

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 SMB at transonic external flow are identified and thrust corrections to the SBM are 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 (Speech)
Additional Information: LIDO-Berichtsjahr=2003,
Title:Influence of transonic Flow on the Thrust Determination of TPS during Wind Tunnel measurements
Authors:
AuthorsInstitution or Email of Authors
Geyr, H. vonUNSPECIFIED
Rossow, C.-C.UNSPECIFIED
Hoheisel, H.UNSPECIFIED
Date:2002
Status:Published
Keywords:TPS thrust determination, CFD, thrust-drag bookkeeping
Event Title:13. DGLR-Fachsymposium der AG STAB, München (de), 12.-14.11.2002
Organizer:DGLR
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes: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 19:07

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