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Providing alternative escape routes:
The first thing to check is if everyone can turn away from the fire and move safely away from it.
For this to be the case there will have to be at least two exits that everyone can get to. Then, if one exit is inaccessible due to the location of the fire, everyone can go to another exit.
The second part of the aim is that people, having turned away from the fire and started to move towards another exit, can move safely away from it. This is stated because it will not be satisfactory if the alternative exit is not large enough to allow everyone to flow through it quickly enough causing a queue to form that endangers the people at the back of the queue.
how to develop an algorithm that will accept the names of sales staff members and the total sales for the month.the algorithm must calculate the commission of 3% of the total sales
AIRCRAFT WEIGHING NOTE: The C.A.A. will consider applications from aircraft constructors and operators to weigh certain types of aircraft on a sampling basis. (i.e. repre
can i get prportional and integral controller matlab coding to solve my load flow analysis
Interior noise is basically airborne or structure-borne. The excitation sources of vibratation and noise from engines can be divided as mechanical, combustion, and flow sources.
FIRING ORDER If in multi cylinder engines, various cylinders are made to fire one after the other, interference between adjacent cylinders would occur, since these may have o
Double acting propellers: This type of propeller is normally fitted to larger engine and, because of engine requirements, is more complicated than the propellers fitted to smal
Fire evacuation - Railway inspections: Fire evacuation signals should be given by voice messages and these must be easily understood by the occupants. The expected populati
Applications of the subject strength of materials
Nozzle Area and Shape Control In a high by-pass ratio engine with a single-stage fan without inlet guide vanes, the predominant sources governing the overall noise level are th
apply equations to solve problems for specified aerodynamic applications. Need some inputs regarding this.
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