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%3A02098621" target="_blank" >RIV/68407700:21220/03:02098621 - isvavai.cz</a>

Result on the web

—

DOI - Digital Object Identifier

—

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 units consists 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 themain difficulty is the deformation of the flow field at the entry to the blower.

Czech name

—

Czech description

—

Type

J_x - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

CEP classification

AM - Pedagogy and education

OECD FORD branch

—

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

Name of the periodical

Acta Polytechnica

ISSN

1210-2709

e-ISSN

—

Volume of the periodical

43

Issue of the periodical within the volume

6

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

6

Pages from-to

3-8

UT code for WoS article

—

EID of the result in the Scopus database

—