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

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F03%3A02091421" target="_blank" >RIV/68407700:21220/03:02091421 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

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

Original language description

So-called "cold-jet" propulsion unit consist of the piston engine, blower and the necessary air duct. Till now, all attempts to utilize "cold-jet" propulsion unit to maintain the trust of airplane were unsuccessful. Analysis has shown that the main difficulty was the deformation of the flow fields at the entry to the blowers.

Czech name

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Czech description

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Type

A - Audiovisual production

CEP classification

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

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Project

<a href="/en/project/LN00B051" target="_blank" >LN00B051: Aerospace research centre (ARC)</a><br>

Continuities

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year

2003

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

ISBN

80-86059-35-9

Place of publication

Praha

Publisher/client name

Not available

Version

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Carrier ID

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