Spelling suggestions: "subject:"aerodynamic resistance"" "subject:"therodynamic resistance""
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Oro srauto pasiskirstymo pagrindiniame ortakyje tyrimai / Air flow distribution in main air channelGaidžiūnaitė, Daiva 02 June 2011 (has links)
Darbo apimtis 42 puslapiai, jame yra 15 paveikslų ir 2 lentelės. Literatūros sąraše 31 šaltiniai(iš jų 11 rusų kalba). Darbo pradžia 2009.09.01 pabaiga 2011.05. Šio darbo tikslas – nustatyti debito koeficiento kitimą išilgai pagrindinio ortakio, priklausomai nuo šoninių ortakių aerodinaminio pasipriešinimo ir tiekiamo oro srauto. Ekspermentinio stendo pagalba nustatyti faktinis oro pasiskirstymas išilgai pagrindinio ortakio. Matematinio modulio pagalba apskaičiuotas teorinis oro pasiskirstymas, kai oras išteka į šoninius ortakius veikiamas statinio slėgio. Išanalizavus rezultatus nustatytas debito koeficiento kitimas išilgai skirstomojo ortakio ir jį įtakojantys veiksniai. / The volume of work contains 42 pages, 15 pictures and 2 tables. In the literature list 31 are sources (of them 11 are russian). The beginning of work – 2009.09.01 and the end – 2011.05. The aim of this paper is to define the variation of yield coefficient along the main channel, depending on the aerodynamic resistance of lateral duct and the flow of the supplied air. With the help of the experimental stand, to define real dissemination of air along the main channel. With the help of the mathematic module, to calculate theoretical dissemination of air, when it flows to lateral duct affected by static pressure. After the analysis of the results, the variation of yield coefficient along the main channel and the influencing factors were defined.
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Development of an Autonomous Flying Insect Scouting System for Greenhouse EnvironmentsBiffi, Alfredo January 2009 (has links)
No description available.
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Návrh letounu podle předpisu FAR 103 / Design of Aircraft in Accordance with FAR 103 RegulationTomala, Daniel January 2008 (has links)
This diploma work considers conceptual design of aircraft in accordance in FAR 103 regulation. On the base of statistical dates has been made basic geometrical and aero-dynamical concept of a single occupant aircraft. For conception have been chosen optimal driving force and bases calculations of the load pressure and dimensions are included.
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