Sökning: WFRF:(Lekholm Ville) > Schlieren Imaging o...
Fältnamn | Indikatorer | Metadata |
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000 | 03367naa a2200409 4500 | |
001 | oai:DiVA.org:uu-186252 | |
003 | SwePub | |
008 | 121128s2012 | |||||||||||000 ||eng| | |
024 | 7 | a https://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-1862522 URI |
024 | 7 | a https://doi.org/10.1088/0957-0233/23/8/0854032 DOI |
040 | a (SwePub)uu | |
041 | a engb eng | |
042 | 9 SwePub | |
072 | 7 | a ref2 swepub-contenttype |
072 | 7 | a art2 swepub-publicationtype |
100 | 1 | a Lekholm, Ville,d 1976-u Uppsala universitet,Mikrosystemteknik,ÅSTC4 aut0 (Swepub:uu)ville816 |
245 | 1 0 | a Schlieren Imaging of Microthruster Exhausts for Qualitative and Quantitative Analysis |
264 | c 2012-05-31 | |
264 | 1 | b Institute of Physics (IOP),c 2012 |
338 | a electronic2 rdacarrier | |
520 | a Abstract. Schlieren imaging is a method used to visualize differences in refractiveindex within a medium. It is a powerful and straightforward tool for sensitiveand high-resolution visualization of, e.g., gas flows. Here, heated cold gasmicrothrusters were studied with this technique. The thrusters are manufacturedusing microelectromechanical systems technology, and measure 22×22×0.85 mm. Thenozzles are approximately 20 µm wide at the throat, and 350 µm wide at the exit.Through these studies, verification of the functionality of the thrusters, and directvisualization and of the thruster exhausts was possible. At atmospheric pressure,slipping of the exhaust was observed, due to severe overexpansion of the nozzle. Invacuum (3 kPa), the exhaust was imaged while feed pressure was varied from 100 to450 kPa. The nozzle was overexpanded, and the flow was seen to be supersonic. Theshock cell period was linearly dependent on feed pressure, ranging from 320 to 610 µm.With activated heaters, the shock cell separation increased. The effect of the heaterswas more prominent at low feed pressure, and an increase in specific impulse of 20%was calculated. It was also shown that schlieren imaging can be used to detect leaks,making it a valuable, safe, and noninvasive aid in quality control of the thrusters. | |
650 | 7 | a TEKNIK OCH TEKNOLOGIERx Annan teknikx Övrig annan teknik0 (SwePub)211992 hsv//swe |
650 | 7 | a ENGINEERING AND TECHNOLOGYx Other Engineering and Technologiesx Other Engineering and Technologies not elsewhere specified0 (SwePub)211992 hsv//eng |
653 | a Schlieren imaging | |
653 | a microthrusters | |
653 | a MEMS | |
653 | a shock cells | |
653 | a Teknisk fysik med inriktning mot mikrosystemteknik | |
653 | a Engineering Science with specialization in Microsystems Technology | |
700 | 1 | a Palmer, Kristofferu Uppsala universitet,Mikrosystemteknik,ÅSTC4 aut0 (Swepub:uu)kripa149 |
700 | 1 | a Thornell, Gregeru Uppsala universitet,Mikrosystemteknik,ÅSTC4 aut0 (Swepub:uu)gth12095 |
710 | 2 | a Uppsala universitetb Mikrosystemteknik4 org |
773 | 0 | t Measurement science and technologyd : Institute of Physics (IOP)g 23:8, s. 085403-q 23:8<085403-x 0957-0233x 1361-6501 |
856 | 4 | u https://uu.diva-portal.org/smash/get/diva2:572764/FULLTEXT02.pdfx primaryx Raw objecty fulltext:postprint |
856 | 4 | u http://uu.diva-portal.org/smash/get/diva2:572764/FULLTEXT02 |
856 | 4 8 | u https://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-186252 |
856 | 4 8 | u https://doi.org/10.1088/0957-0233/23/8/085403 |
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