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Description
  • Prezentace vztlakových křivek, polárů a momentových křivek profilu MS13013, který byl vytvořen symetrizací zadní části profilu NASA MS(1)-0313. Byla sklápěna náběžná hrana, měřilo se při Reynoldsově čísle 1,7x106. Potvrdila se starší zkušenost a výsledkyvýpočtů programem XFOIL, že u tohoto profilu se horní vrchol vztlakové křivky a kritický úhel náběhu sklápěním náběžné hrany proti očekávání nezvýší, kdežto dolní část vztlakové křivky se podle očekávání pokazí. Tyto výsledky jsou asi platné pro všechnyprofily typu MS. (cs)
  • Presentation of the measured lift curves, lift-drag and lift-moment characteristics of an MS13013 airfoil. The airfoil was created from NASA MS(1)-0313 airfoil by symmetrisation of its rear part. The leading edge was lowered to three positions. Reynoldsnumber was 1.7x106. The older experience and computational results using the XFOIL code have been verified to show that in this airfoil the lift curve upper peak and the stall angle of attack will not increase as might be expected whilst the lift curve lower part gets worse as expected. These results are apparently valid for any airfoils whose front part is taken from MS(1)-031X airfoils.
  • Presentation of the measured lift curves, lift-drag and lift-moment characteristics of an MS13013 airfoil. The airfoil was created from NASA MS(1)-0313 airfoil by symmetrisation of its rear part. The leading edge was lowered to three positions. Reynoldsnumber was 1.7x106. The older experience and computational results using the XFOIL code have been verified to show that in this airfoil the lift curve upper peak and the stall angle of attack will not increase as might be expected whilst the lift curve lower part gets worse as expected. These results are apparently valid for any airfoils whose front part is taken from MS(1)-031X airfoils. (en)
Title
  • Measured Aerodynamic Characteristics of MS13013 Airfoil with Inclinable Leading Edge
  • Změřené aerodynamické charakteristiky profilu MS13013 se sklonnou náběžnou hranou (cs)
  • Measured Aerodynamic Characteristics of MS13013 Airfoil with Inclinable Leading Edge (en)
skos:prefLabel
  • Measured Aerodynamic Characteristics of MS13013 Airfoil with Inclinable Leading Edge
  • Změřené aerodynamické charakteristiky profilu MS13013 se sklonnou náběžnou hranou (cs)
  • Measured Aerodynamic Characteristics of MS13013 Airfoil with Inclinable Leading Edge (en)
skos:notation
  • RIV/00010669:_____/04:#0000114!RIV06-MSM-00010669
http://linked.open.../vavai/riv/strany
  • 2;4
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • Z(MSM0001066901)
http://linked.open...iv/cisloPeriodika
  • 2
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
  • 572582
http://linked.open...ai/riv/idVysledku
  • RIV/00010669:_____/04:#0000114
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • Measured Aerodynamic Characteristics; Airfoil; Inclinable Leading Edge (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...odStatuVydavatele
  • CZ - Česká republika
http://linked.open...ontrolniKodProRIV
  • [3F362F610DD7]
http://linked.open...i/riv/nazevZdroje
  • Letecký zpravodaj - Czech Aerospace Proceedings
http://linked.open...in/vavai/riv/obor
http://linked.open...ichTvurcuVysledku
http://linked.open...cetTvurcuVysledku
http://linked.open...UplatneniVysledku
http://linked.open...v/svazekPeriodika
  • 2/2004
http://linked.open...iv/tvurceVysledku
  • Berák, Petr
http://linked.open...n/vavai/riv/zamer
issn
  • 1211-877X
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