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Investigation of the installation Effects of an Ultra High Bypass Engine Type

Schenk, M. (1995) Investigation of the installation Effects of an Ultra High Bypass Engine Type. DLR-Interner Bericht. 129-95/3. DLR Braunschweig. 114 S.

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This document presents the results of analysis of the tests with ALVAST and CRUF at different power settings at the Mach numbers 0.18, 0.27 and 0.34. The pressure distribution at the wing sections is shown at different angles of attack and thrust conditions. In addition the effects of thrust and Mach number on wing pressure distribution, local lift, overall lift and drag are shown. Also investigated are the effects of thrust and Mach number on nacelle, pylon and fuselage, with the most attention being payed to the influence on the nacelle. Finally a comparison of TPS and CRUF measurements shows directly the advantages or disadvantages of CRUF compared with conventional propulsions (TPS) and Clean configurations. It is shown for wing pressure distribution,local lift at wing sections, overall lift and drag.

Item URL in elib:https://elib.dlr.de/36355/
Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1995,
Title:Investigation of the installation Effects of an Ultra High Bypass Engine Type
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Open Access:No
Number of Pages:114
Keywords:Transport aircraft, ALVAST, Turbine Powered Simulator, Ultra High Bypass Engine, CRUF, pressure coefficient, lift, drag
Institution:DLR Braunschweig
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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