About: Contribution to the Solution of Thermal Stress in Cylindrical Wall of the Solid Propellant Rocket Motor.     Goto   Sponge   NotDistinct   Permalink

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  • The article deals with the thermal load of solid propellant rocket motor combustion chamber. In contribution the case of thermal stress of the cylindrical wall is analysed when the solid propellant rocket motor has the short time of action. Thermal stress is a consequence of solid propellant rocket motor charge burning. For this analyzes the thermal load is estimated from an experiment. The stresses are assessed in meridional and hoop directions. Cylindrical part of the combustion chamber is closed on one end by rigid plate and is considered as a shell construction. The pressure and thermal load are axisymmetrical. The new in this paper is evaluation of the thermo camera usage for the temperature fields estimation on the combustion chamber construction during experiments.
  • The article deals with the thermal load of solid propellant rocket motor combustion chamber. In contribution the case of thermal stress of the cylindrical wall is analysed when the solid propellant rocket motor has the short time of action. Thermal stress is a consequence of solid propellant rocket motor charge burning. For this analyzes the thermal load is estimated from an experiment. The stresses are assessed in meridional and hoop directions. Cylindrical part of the combustion chamber is closed on one end by rigid plate and is considered as a shell construction. The pressure and thermal load are axisymmetrical. The new in this paper is evaluation of the thermo camera usage for the temperature fields estimation on the combustion chamber construction during experiments. (en)
  • Článek pojednává o problematice teplotního zatížení spalovací komory raketového motoru. V příspěvku je analyzován případ vzniku teplotního napětí ve válcové stěně raketového motoru s kratší dobou funkce. Teplotní napětí je důsledek hoření náplně raketového motoru na tuhou pohonnou hmotu . Pro tuto analýzu je teplotní pole odhadováno z experimentu. Napětí je posuzováno v osovém a obvodovém směru. Válcová část spalovací komory je uzavřena tuhou deskou a je uvažována jako skořepinová konstrukce. Tlakové i teplotní zatížení je osově symetrické. (cs)
Title
  • Contribution to the Solution of Thermal Stress in Cylindrical Wall of the Solid Propellant Rocket Motor.
  • Contribution to the Solution of Thermal Stress in Cylindrical Wall of the Solid Propellant Rocket Motor. (en)
  • Příspěvek k řešení teplotního napětí ve válcové stěně raketového motoru na tuhou pohonnou hmotu. (cs)
skos:prefLabel
  • Contribution to the Solution of Thermal Stress in Cylindrical Wall of the Solid Propellant Rocket Motor.
  • Contribution to the Solution of Thermal Stress in Cylindrical Wall of the Solid Propellant Rocket Motor. (en)
  • Příspěvek k řešení teplotního napětí ve válcové stěně raketového motoru na tuhou pohonnou hmotu. (cs)
skos:notation
  • RIV/60162694:G43__/08:#0001830!RIV09-MO0-G43_____
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • Z(MO0FVT0000404)
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
  • 361224
http://linked.open...ai/riv/idVysledku
  • RIV/60162694:G43__/08:#0001830
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • Solid Propellant Rocket Motor; Combustion Chamber; Thermal Stress (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...ontrolniKodProRIV
  • [B056C46E0DF4]
http://linked.open...v/mistoKonaniAkce
  • Pułtusk (Polsko)
http://linked.open...i/riv/mistoVydani
  • Warsawa
http://linked.open...i/riv/nazevZdroje
  • Scientific Aspects of Armament & Safety Technology
http://linked.open...in/vavai/riv/obor
http://linked.open...ichTvurcuVysledku
http://linked.open...cetTvurcuVysledku
http://linked.open...UplatneniVysledku
http://linked.open...iv/tvurceVysledku
  • Machala, Milan
  • Rovenský, Anton
http://linked.open...vavai/riv/typAkce
http://linked.open.../riv/zahajeniAkce
http://linked.open...n/vavai/riv/zamer
number of pages
http://purl.org/ne...btex#hasPublisher
  • Wojskowa Akademia Techniczna
https://schema.org/isbn
  • 978-83-89399-95-3
http://localhost/t...ganizacniJednotka
  • G43
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