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Tools for the Experimental Study of the Integration of Ultra-High Bypass Engines in Transport Aircraft

Kiock, R. (1994) Tools for the Experimental Study of the Integration of Ultra-High Bypass Engines in Transport Aircraft. Proceedings 18th AIAA Aerospace Ground Testing Conference June 20/23, 1994, Colorado Springs, USA.

Full text not available from this repository.

Abstract

A comprehensive program has been executed to develop test hardware for investigating in a wind tunnel test the engine/airframe integration for ultra high bypass ratio engines (UHBR). The new hardware existed of compressed air powered simulators for turbofan and UHBR engines jointly with the necessary new auxilliary systems. The other hardware needed for the wind tunnel test was already available and included one simulator of both types and a twin-engine transport aircraft. During the acceptance test and the subsequent calibration of the simulators, the new hardware proved that it fulfilled its expectations. Detailed information was obtained from the wind tunnel test showing how the engine flow affects the flow field around the airframe. This proved that powered engine simulators are useful tools for engine/airframe interference investigations.

Item URL in elib:https://elib.dlr.de/36240/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1994, pages=18,
Title:Tools for the Experimental Study of the Integration of Ultra-High Bypass Engines in Transport Aircraft
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Kiock, R.UNSPECIFIEDUNSPECIFIED
Date:1994
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Engine/Airframe interference, surface pressure measurements, balance measurements, testing requirements
Event Title:Proceedings 18th AIAA Aerospace Ground Testing Conference June 20/23, 1994, Colorado Springs, USA
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):L - Concepts & Integration (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: DLR-Beauftragter, elib
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:05

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