About: Analysis of Twin Turboprop Aircraft Whirl-Flutter Stability Boundaries     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
rdfs:seeAlso
Description
  • This paper deals with aircraft structure whirl flutter analysis. It gives a summary of the requirements of airworthiness regulations, the theoretical background and aircraft certification-related issues. The focus is on the whirl flutter analyses of the new Czech twin turboprop utility aircraft. Ordinary and optimization based analytical approaches are described. An optimization based analytical procedure to determine the whirl flutter stability boundaries for certification speed is employed. Analyses include nominal state calculation and evaluation of the influence of secondary parameters to whirl flutter stability. Finally, the propeller – nacelle – wing interference effects (downwash) are evaluated and future work is outlined.
  • This paper deals with aircraft structure whirl flutter analysis. It gives a summary of the requirements of airworthiness regulations, the theoretical background and aircraft certification-related issues. The focus is on the whirl flutter analyses of the new Czech twin turboprop utility aircraft. Ordinary and optimization based analytical approaches are described. An optimization based analytical procedure to determine the whirl flutter stability boundaries for certification speed is employed. Analyses include nominal state calculation and evaluation of the influence of secondary parameters to whirl flutter stability. Finally, the propeller – nacelle – wing interference effects (downwash) are evaluated and future work is outlined. (en)
Title
  • Analysis of Twin Turboprop Aircraft Whirl-Flutter Stability Boundaries
  • Analysis of Twin Turboprop Aircraft Whirl-Flutter Stability Boundaries (en)
skos:prefLabel
  • Analysis of Twin Turboprop Aircraft Whirl-Flutter Stability Boundaries
  • Analysis of Twin Turboprop Aircraft Whirl-Flutter Stability Boundaries (en)
skos:notation
  • RIV/00010669:_____/13:#0001549!RIV14-MPO-00010669
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • I
http://linked.open...iv/cisloPeriodika
  • 6
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
  • 60735
http://linked.open...ai/riv/idVysledku
  • RIV/00010669:_____/13:#0001549
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • aeroelasticity; flutter; whirl flutter (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...odStatuVydavatele
  • US - Spojené státy americké
http://linked.open...ontrolniKodProRIV
  • [B7EB6F25A431]
http://linked.open...i/riv/nazevZdroje
  • Journal of Aircraft
http://linked.open...in/vavai/riv/obor
http://linked.open...ichTvurcuVysledku
http://linked.open...cetTvurcuVysledku
http://linked.open...UplatneniVysledku
http://linked.open...v/svazekPeriodika
  • 49
http://linked.open...iv/tvurceVysledku
  • Čečrdle, Jiří
http://linked.open...ain/vavai/riv/wos
  • 000312764000014
issn
  • 0021-8669
number of pages
http://bibframe.org/vocab/doi
  • 10.2514/1.C031390
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