Numerical investigations for an optimal mounting position of intakes for the air conditioning unit

Voß, Guido (2008) Numerical investigations for an optimal mounting position of intakes for the air conditioning unit. STAB, 2008-11-03 - 2008-11-04, Aachen (Deutschland). (Submitted)

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Abstract

This article presents the results of calculations of a generic medium range aircraft with air intakes and ducts in comparison to a reference aircraft configuration. Main goal of the investigations is to detect an optimal mounting position of the intake unit inside the fuselage regarding pressure coefficient c<sub>p</sub>, total pressure coefficient "eta" and distorsion "DC". It could be shown that there is an impact of the flow conditions in environment of the intake unit to the aerodynamics around the aircraft geometry.

Document Type:

Conference or Workshop Item (Speech, Paper)

Title:

Numerical investigations for an optimal mounting position of intakes for the air conditioning unit

Authors:

Authors	Institution or Email of Authors
Voß, Guido

Date:

November 2008

Refereed publication:

Yes

In ISI Web of Science:

Status:

Submitted

Keywords:

air coditioning, intake, duct, medium range aircraft

Event Title:

STAB

Event Location:

Aachen (Deutschland)

Event Type:

national Conference

Event Dates:

2008-11-03 - 2008-11-04

Organizer:

RWTH Aachen

HGF - Research field:

Aeronautics, Space and Transport

HGF - Program:

Aeronautics

HGF - Program Themes:

L - no assignement

DLR - Research area:

Aeronautics

DLR - Program:

L - no assignement

DLR - Research theme (Project):

["eprint_fieldopt_dlr_project_search_L000" not defined]

Location:

Braunschweig

Institutes and Institutions:

Institute of Aerodynamics and Flow Technology

Deposited By:

Guido Voß

Deposited On:

30 Jan 2009

Last Modified:

27 Apr 2009 15:42

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