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Description
  • The paper deals with the description of the Ground Vibration Test unit for of small aeroplanes and gliders up to the maximum takeoff weight 650 kg. The equipment is developed in terms of the task Research Development of Aircraft Composite Structures of the project Aerospace Research Centre. This article gives information of a measuring Unit and shows comparison of results of Ground Vibration Test on sailplane HPH 304 CZ.
  • The paper deals with the description of the Ground Vibration Test unit for of small aeroplanes and gliders up to the maximum takeoff weight 650 kg. The equipment is developed in terms of the task Research Development of Aircraft Composite Structures of the project Aerospace Research Centre. This article gives information of a measuring Unit and shows comparison of results of Ground Vibration Test on sailplane HPH 304 CZ. (en)
  • Příspěvek popisuje zařízení pro pozemní frekvenční zkoušky lehkých letadel a jeho použití při měření frekvenčních charakteristik kluzáku HPH 304 CZ. (cs)
Title
  • The Ground Vibration Test Stand for Small Sport Aircraft
  • The Ground Vibration Test Stand for Small Sport Aircraft (en)
  • Zařízení pro pozemní frekvenční zkoušky lehkých letadel (cs)
skos:prefLabel
  • The Ground Vibration Test Stand for Small Sport Aircraft
  • The Ground Vibration Test Stand for Small Sport Aircraft (en)
  • Zařízení pro pozemní frekvenční zkoušky lehkých letadel (cs)
skos:notation
  • RIV/68407700:21220/06:02128684!RIV07-MSM-21220___
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  • 477324
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  • RIV/68407700:21220/06:02128684
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  • aeroelasticity; flutter; frequency test; small airplanes (en)
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  • [01F9A717E63D]
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  • Praha
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  • Slavík, Svatomír
  • Kostroun, Tomáš
  • Weigel, Karel
https://schema.org/isbn
  • 80-86059-44-8
http://localhost/t...ganizacniJednotka
  • 21220
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