%0 Journal Article
%T Mathematical model of unsteady air outflow from compartment §®§Ñ§ä§Ö§Þ§Ñ§ä§Ú§é§Ö§ã§Ü§Ñ§ñ §Þ§à§Õ§Ö§Ý§î §ß§Ö§ã§ä§Ñ§è§Ú§à§ß§Ñ§â§ß§à§Ô§à §á§â§à§è§Ö§ã§ã§Ñ §Ú§ã§ä§Ö§é§Ö§ß§Ú§ñ §Ó§à§Ù§Õ§å§ç§Ñ §Ú§Ù §à§ä§ã§Ö§Ü§Ñ §®§¡§´§¦§®§¡§´§ª§¹§¯§¡ §®§°§¥§¦§­§¾ §¯§¦§³§´§¡§¸ §°§¯§¡§²§¯§°§¤§° §±§²§°§¸§¦§³§µ §£§ª§´ §¬§¡§¯§¯§Á §±§°§£ §´§²§Á §© §£ §¥§³ §¬§µ
%A §£.§¥. §¥§à§ß§Ú§Ü
%J Proceedings of National Aviation University
%D 2005
%I National Aviation University
%X The mathematical model of gas efflux from large volume bay regarding gas braking parameters has been developed. Influence of parameters of air which inflows and outflows on parameters of air inside a compartment is investigated.  §²§Ñ§Ù§â§Ñ§Ò§à§ä§Ñ§ß§Ñ §Þ§Ñ§ä§Ö§Þ§Ñ§ä§Ú§é§Ö§ã§Ü§Ñ§ñ §Þ§à§Õ§Ö§Ý§î §à§á§â§Ö§Õ§Ö§Ý§Ö§ß§Ú§ñ §Õ§Ñ§Ó§Ý§Ö§ß§Ú§ñ §Ú §ä§Ö§Þ§á§Ö§â§Ñ§ä§å§â§í §Ó§à§Ù§Õ§å§ç§Ñ §Ó §Ù§Ñ§ä§à§â§Þ§à§Ø§Ö§ß§ß§à§Þ §á§à§ä§à§Ü§Ö §Ó§ß§å§ä§â§Ú §à§ä§ã§Ö§Ü§Ñ §á§â§Ú §á§à§Õ§Ó§à§Õ§Ö §Ú §à§ä§Ó§à§Õ§Ö §Ó§à§Ù§Õ§å§ç§Ñ. §±§â§à§Ó§Ö§Õ§Ö§ß§í §Ú§ã§ã§Ý§Ö§Õ§à§Ó§Ñ§ß§Ú§ñ §Ó§Ý§Ú§ñ§ß§Ú§ñ §á§Ñ§â§Ñ§Þ§Ö§ä§â§à§Ó §á§à§Õ§Ó§à§Õ§Ú§Þ§à§Ô§à §Ú §à§ä§Ó§à§Õ§Ú§Þ§à§Ô§à §Ó§à§Ù§Õ§å§ç§Ñ §ß§Ñ §á§Ñ§â§Ñ§Þ§Ö§ä§â§í §Ó§à§Ù§Õ§å§ç§Ñ §Ó§ß§å§ä§â§Ú §à§ä§ã§Ö§Ü§Ñ.  §²§à§Ù§â§à§Ò§Ý§Ö§ß§à §Þ§Ñ§ä§Ö§Þ§Ñ§ä§Ú§é§ß§å §Þ§à§Õ§Ö§Ý§î §Ó§Ú§Ù§ß§Ñ§é§Ö§ß§ß§ñ §ä§Ú§ã§Ü§å   §ä§Ö§Þ§á§Ö§â§Ñ§ä§å§â§Ú §á§à§Ó §ä§â§ñ §Ó §Ù§Ñ§Ô§Ñ§Ý§î§Þ§à§Ó§Ñ§ß§à§Þ§å §á§à§ä§à§è  §Ó §ã§Ö§â§Ö§Õ§Ú§ß  §Ó §Õ§ã §Ü§å §á§â§Ú §á §Õ§Ó§Ö§Õ§Ö§ß§ß    §Ó §Õ§Ó§Ö§Õ§Ö§ß§ß  §á§à§Ó §ä§â§ñ. §±§â§à§Ó§Ö§Õ§Ö§ß§à §Õ§à§ã§Ý §Õ§Ø§Ö§ß§ß§ñ §Ó§á§Ý§Ú§Ó§å §á§Ñ§â§Ñ§Þ§Ö§ä§â §Ó §á §Õ§Ó §Õ§ß§à§Ô§à   §Ó §Õ§Ó §Õ§ß§à§Ô§à §á§à§Ó §ä§â§ñ §ß§Ñ §á§Ñ§â§Ñ§Þ§Ö§ä§â§Ú §á§à§Ó §ä§â§ñ §Ó §ã§Ö§â§Ö§Õ§Ú§ß  §Ó §Õ§ã §Ü§å.
%U http://jrnl.nau.edu.ua/index.php/visnik/article/view/1114