Inlet Channel for a Ducted Fan Propulsion System of a Light Aircraft

So-called "cold-jet" propulsion units consist of a piston engine, a blower and the necessary air duct. Till now, all attempts to utilize "cold-jet" propulsion units to maintain the thrust of an airplane have been unsuccessful. Analysis has shown that the main difficulty is the de...

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Bibliographic Details
Main Authors: E. Ritschl, R. Theiner, D. Hanus
Format: Article
Language:English
Published: CTU Central Library 2003-01-01
Series:Acta Polytechnica
Subjects:
Online Access:https://ojs.cvut.cz/ojs/index.php/ap/article/view/486
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spelling doaj-f2e8aa56cd664b878b2713d8991397582020-11-24T22:48:01ZengCTU Central LibraryActa Polytechnica1210-27091805-23632003-01-01436486Inlet Channel for a Ducted Fan Propulsion System of a Light AircraftE. RitschlR. TheinerD. HanusSo-called "cold-jet" propulsion units consist of a piston engine, a blower and the necessary air duct. Till now, all attempts to utilize "cold-jet" propulsion units to maintain the thrust of an airplane have been unsuccessful. Analysis has shown that the main difficulty is the deformation of the flow field at the entry to the blower [1].https://ojs.cvut.cz/ojs/index.php/ap/article/view/486aircraftducted fancold-jetinlet channelaerodynamics
collection DOAJ
language English
format Article
sources DOAJ
author E. Ritschl
R. Theiner
D. Hanus
spellingShingle E. Ritschl
R. Theiner
D. Hanus
Inlet Channel for a Ducted Fan Propulsion System of a Light Aircraft
Acta Polytechnica
aircraft
ducted fan
cold-jet
inlet channel
aerodynamics
author_facet E. Ritschl
R. Theiner
D. Hanus
author_sort E. Ritschl
title Inlet Channel for a Ducted Fan Propulsion System of a Light Aircraft
title_short Inlet Channel for a Ducted Fan Propulsion System of a Light Aircraft
title_full Inlet Channel for a Ducted Fan Propulsion System of a Light Aircraft
title_fullStr Inlet Channel for a Ducted Fan Propulsion System of a Light Aircraft
title_full_unstemmed Inlet Channel for a Ducted Fan Propulsion System of a Light Aircraft
title_sort inlet channel for a ducted fan propulsion system of a light aircraft
publisher CTU Central Library
series Acta Polytechnica
issn 1210-2709
1805-2363
publishDate 2003-01-01
description So-called "cold-jet" propulsion units consist of a piston engine, a blower and the necessary air duct. Till now, all attempts to utilize "cold-jet" propulsion units to maintain the thrust of an airplane have been unsuccessful. Analysis has shown that the main difficulty is the deformation of the flow field at the entry to the blower [1].
topic aircraft
ducted fan
cold-jet
inlet channel
aerodynamics
url https://ojs.cvut.cz/ojs/index.php/ap/article/view/486
work_keys_str_mv AT eritschl inletchannelforaductedfanpropulsionsystemofalightaircraft
AT rtheiner inletchannelforaductedfanpropulsionsystemofalightaircraft
AT dhanus inletchannelforaductedfanpropulsionsystemofalightaircraft
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