Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Predrag Stojakovic"'
Autor:
Predrag Stojakovic, Bosko Rasuo
Publikováno v:
Aircraft Engineering and Aerospace Technology: An International Journal, 2016, Vol. 88, Issue 1, pp. 42-52.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-03-2014-0033
Autor:
Miguel A. Valverde, René Böttcher, Selma A. Serra, Pablo Latorre, David Canadell, Jason Moffat, Francesc Posas, Predrag Stojakovic, Eulàlia de Nadal, Michael Aregger, Fanny Rubio-Moscardo, Ramon Amat, Gerhard Seisenbacher
Publikováno v:
Proc Natl Acad Sci U S A
Regulation of cell volume is essential for tissue homeostasis and cell viability. In response to hypertonic stress, cells need rapid electrolyte influx to compensate water loss and to prevent cell death in a process known as regulatory volume increas
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bb2b07b94696b7c9ffa83c65e1c22132
http://hdl.handle.net/10230/48308
http://hdl.handle.net/10230/48308
Autor:
Predrag Stojakovic, Boško Rašuo
Publikováno v:
Aerospace Science and Technology. 49:239-249
This paper presents the application of the previously presented general analysis method to determine the safe flight boundaries of the asymmetrically loaded airplane within the terminal flight phases as applied to the case of inherently asymmetric si
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8b4142d7ca8b9a50454dbfe79ffcee78
https://doi.org/10.1016/j.ast.2015.12.012
https://doi.org/10.1016/j.ast.2015.12.012
Autor:
Boško Rašuo, Predrag Stojakovic
Publikováno v:
Aircraft Engineering and Aerospace Technology. 88:42-52
Purpose – The purpose of this paper is to present a method for determining the safe flight boundaries of the asymmetrically loaded airplane in the terminal flight phases. The method is applicable to both, the inherent airplane asymmetries and those
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::162cd554748e54cfcb7a0bc1c767d604
https://doi.org/10.1108/aeat-03-2014-0033
https://doi.org/10.1108/aeat-03-2014-0033
Publikováno v:
Aerospace Science and Technology. 46:227-235
This paper presents the analysis of effects on the airplane longitudinal stability reserve by the single tractor propeller at high engine power settings. The analysis was done within the terminal flight phases. The airplane has the original and modif
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b757b85fdfe02ef751843cc6ed50a127
https://doi.org/10.1016/j.ast.2015.07.017
https://doi.org/10.1016/j.ast.2015.07.017
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 53:130-137
The paper presents a new approach to analysis of dynamic properties of the rotating airplane. The analysis is based on the rate of rotational energy and a full non-linear model of airplane dynamics. It can be applied to a whole range of attack angles
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e09bd2d8673a12c915a464eb7dcac394
https://doi.org/10.2322/tjsass.53.130
https://doi.org/10.2322/tjsass.53.130