About: Composite Axial Flow Propulsor of Small Aircraft     Goto   Sponge   NotDistinct   Permalink

An Entity of Type : http://linked.opendata.cz/ontology/domain/vavai/Vysledek, within Data Space : linked.opendata.cz associated with source document(s)

AttributesValues
rdf:type
Description
  • Není k dispozici (cs)
  • Work is focused on many aspects of design of axial flow, one stage, ducted fan driven by four stroke, four cylinder reciprocating engine Yamaha with the power output of 110 kW. Airplane with this propulsion is expected to be of considerably low drag, because of location of fan inside the hull which will make the airplane aerodynamically smoother compared with classic airplanes with tractor propeller. Such solution minimizes turbulization (disturbance) of the flow around the aircraft so significant part of the airplane wetted surface is expected to work in laminar regime. This fan is of rotor - stator configuration. The need of low weight of fan is reason for choice of carbon/epoxy composite material for blades and driving shaft connecting engine with the fan.
  • Work is focused on many aspects of design of axial flow, one stage, ducted fan driven by four stroke, four cylinder reciprocating engine Yamaha with the power output of 110 kW. Airplane with this propulsion is expected to be of considerably low drag, because of location of fan inside the hull which will make the airplane aerodynamically smoother compared with classic airplanes with tractor propeller. Such solution minimizes turbulization (disturbance) of the flow around the aircraft so significant part of the airplane wetted surface is expected to work in laminar regime. This fan is of rotor - stator configuration. The need of low weight of fan is reason for choice of carbon/epoxy composite material for blades and driving shaft connecting engine with the fan. (en)
Title
  • Není k dispozici (cs)
  • Composite Axial Flow Propulsor of Small Aircraft
  • Composite Axial Flow Propulsor of Small Aircraft (en)
skos:prefLabel
  • Není k dispozici (cs)
  • Composite Axial Flow Propulsor of Small Aircraft
  • Composite Axial Flow Propulsor of Small Aircraft (en)
skos:notation
  • RIV/68407700:21220/04:02102567!RIV/2005/MSM/212205/N
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • P(LN00B051)
http://linked.open...vai/riv/dodaniDat
http://linked.open...aciTvurceVysledku
http://linked.open.../riv/druhVysledku
http://linked.open...iv/duvernostUdaju
http://linked.open...titaPredkladatele
http://linked.open...dnocenehoVysledku
  • 558423
http://linked.open...ai/riv/idVysledku
  • RIV/68407700:21220/04:02102567
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • aircraft propulsion; composite materials; compressor blade; ducted fan; internal aerodynamics (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...i/riv/kodPristupu
http://linked.open...ontrolniKodProRIV
  • [E62DB071EABD]
http://linked.open...i/riv/mistoVydani
  • Praha
http://linked.open...n/vavai/riv/nosic
  • neuvedeno
http://linked.open...in/vavai/riv/obor
http://linked.open...ichTvurcuVysledku
http://linked.open...cetTvurcuVysledku
http://linked.open...vavai/riv/projekt
http://linked.open...UplatneniVysledku
http://linked.open...iv/tvurceVysledku
  • Hanus, Daniel
  • Poul, Robin
https://schema.org/isbn
  • 80-86059-41-3
http://localhost/t...ganizacniJednotka
  • 21220
Faceted Search & Find service v1.16.118 as of Jun 21 2024


Alternative Linked Data Documents: ODE     Content Formats:   [cxml] [csv]     RDF   [text] [turtle] [ld+json] [rdf+json] [rdf+xml]     ODATA   [atom+xml] [odata+json]     Microdata   [microdata+json] [html]    About   
This material is Open Knowledge   W3C Semantic Web Technology [RDF Data] Valid XHTML + RDFa
OpenLink Virtuoso version 07.20.3240 as of Jun 21 2024, on Linux (x86_64-pc-linux-gnu), Single-Server Edition (126 GB total memory, 58 GB memory in use)
Data on this page belongs to its respective rights holders.
Virtuoso Faceted Browser Copyright © 2009-2024 OpenLink Software