Zobrazeno 1 - 10 of 87 pro vyhledávání: '"J. Nožička"'
1
Akademický článek
Computational Simulation of the Flow Past an Airfoil for an Unmanned Aerial Vehicle
Autor: L. Velázquez-Araque, J. Nožička
Publikováno v: Journal of Systemics, Cybernetics and Informatics, Vol 11, Iss 6, Pp 40-46 (2013)
This paper deals with the numerical simulation of the two-dimensional, incompressible, steady air flow past a NACA 2415 airfoil and four modifications of this one. The modification of this airfoil was made in order to create a blowing outlet with the
Externí odkaz: https://doaj.org/article/b890ca223a0f451fb2cf010d62e757ed
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2
Akademický článek
Measurement of Two Phase Flow
Autor: J. Novotný, J. Nožička, J. Adamec, L. Nováková
Publikováno v: Acta Polytechnica, Vol 45, Iss 3 (2005)
This paper presents the results of experiments with moist wet steam. The aim of the experiment was to measure the velocity of the growth of a condensing nucleus in wet steam dependent on the velocity of condensation. For the experiments in wet steam
Externí odkaz: https://doaj.org/article/ef14ae536efc4a519b8e5d7b33d38d07
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3
Implementing Cloud Solutions to Optimize the Operation of District Heating Networks with Preparation for MindSphere®
Autor: P. Sláma, J. Nožička
Publikováno v: Acta Mechanica Slovaca. 25:42-50
The paper describes the data mining within district heating environment (physical data - temperatures and flow rates) as a basis of control and optimization of a particular district heating region. The cycle is defined: the gained data transmission t
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::44a237d7774bf4ddc8cddbe4cd2b510d
https://doi.org/10.21496/ams.2021.007
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6
Design Of An Aerodynamic Measurement System For Unmanned Aerial Vehicle Airfoils
Autor: L. Velázquez-Araque, J. Nožička
Publikováno v: Journal of Systemics, Cybernetics and Informatics, Vol 10, Iss 5, Pp 39-44 (2012)
This paper presents the design and validation of a measurement system for aerodynamic characteristics of unmanned aerial vehicles. An aerodynamic balance was designed in order to measure the lift, drag forces and pitching moment for different airfoil
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doajarticles::d665c97cb6f3001b565d4c375b31a67e
http://www.iiisci.org/Journal/CV$/sci/pdfs/HFA750PV.pdf
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7
Particle image velocimetry investigation of an aerofoil with a Gurney flap
Autor: P Bárta, J Nožička, M Matějka
Publikováno v: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 222:23-28
The current paper reviews the research on NACA 23012 and FX66-17AII-182 aerofoils, aerodynamic performance for different angles of attack at Reynolds number Re ≍ 3 × 105, based on chord, both with clean configuration and the flaps. Flow field arou
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::fc46c9123e19a63b8e62dea7ba3d4dea
https://doi.org/10.1243/09544100jaero267
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9
Radiation pneumonitis: The model of interstitial edema
Autor: Jan Österreicher, J. Nožička, P. Petýrek, Vávrová J, Jiří Knížek
Publikováno v: Experimental and Toxicologic Pathology. 51:491-493
Summary We used the measurement of the thickness of alveolar septa in the lungs in (C57BI/6xDBA/2)F 1 mice irradiated locally in the area of the thorax with absorbed doses of 14, 16 and 18 Gy of gamma rays. The thickness of alveolar septa of the pulm
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e5cbf134ac33bd7f40d0fc4330a41fd3
https://doi.org/10.1016/s0940-2993(99)80122-5
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