Měření letových veličin v akrobatických manévrech

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F06%3APU62400" target="_blank" >RIV/00216305:26210/06:PU62400 - isvavai.cz</a>

Výsledek na webu

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DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

Measurement of aerobatic flight characteristics

Popis výsledku v původním jazyce

Determination of flight parameters in non-steady turns (e.g. aerobatic manoeuvres, stalls, spins) is one of the most complicated tasks within the flight measurement, from the point of view of character of performance and aircraft equipment. Limitary parameters of flight for components of aerobatic manoeuvres are integral part of technical documentation of corresponding aircraft category. According to the Airworthiness standards, aerobatic and training aircraft classes have to have the ability to do safee aerobatic turns that requires type certificate. There are measurements, done within the flight measurements at the Institute of Aerospace Engineering in Brno, which made possible to monitor the whole aerobatic configuration of the two-seat, all-metal sailplane L-13 AC Blaník. During the test flights, the basic aerobatic elements, such as loop, stall turn, inverted flight, roll, etc., were done with the sailplane. It was necessary to equip the aircraft with the measurement technology ca

Název v anglickém jazyce

Measurement of aerobatic flight characteristics

Popis výsledku anglicky

Determination of flight parameters in non-steady turns (e.g. aerobatic manoeuvres, stalls, spins) is one of the most complicated tasks within the flight measurement, from the point of view of character of performance and aircraft equipment. Limitary parameters of flight for components of aerobatic manoeuvres are integral part of technical documentation of corresponding aircraft category. According to the Airworthiness standards, aerobatic and training aircraft classes have to have the ability to do safee aerobatic turns that requires type certificate. There are measurements, done within the flight measurements at the Institute of Aerospace Engineering in Brno, which made possible to monitor the whole aerobatic configuration of the two-seat, all-metal sailplane L-13 AC Blaník. During the test flights, the basic aerobatic elements, such as loop, stall turn, inverted flight, roll, etc., were done with the sailplane. It was necessary to equip the aircraft with the measurement technology ca

Druh

D - Stať ve sborníku

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

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Projekt

<a href="/cs/project/1M0501" target="_blank" >1M0501: Centrum leteckého a kosmického výzkumu</a><br>

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Rok uplatnění

2006

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název statě ve sborníku

4th International PhD Conference on Mechanical Engineering - PhD2006

ISBN

80-7043-486-4

ISSN

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e-ISSN

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Počet stran výsledku

6

Strana od-do

41-46

Název nakladatele

NEUVEDEN

Místo vydání

Plzeň

Místo konání akce

University of West Bohemia, Faculty of Mechanica

Datum konání akce

11. 9. 2006

Typ akce podle státní příslušnosti

CST - Celostátní akce

Kód UT WoS článku

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