Answer:
moment of inertia = 4.662 * 10^6 
Explanation:
Given data :
Mass of machine = 400 kg = 400 * 9.81 = 3924 N
length of span = 3.2 m
E = 200 * 10^9 N/m^2
frequency = 9.3 Hz
Wm ( angular frequency ) = 2
= 58.434 rad/secs
also Wm =
------- EQUATION 1
g = 9.81
deflection of simply supported beam
t = 
insert the value of t into equation 1
W
=
make I the subject of the equation
I ( Moment of inertia about the neutral axis ) = 
I =
= 4.662 * 10^6 
Using an appropriate failure theory, find the factor of safety in each case. State the name of the theory that you are using the theory is max stress theory.
<h3>Wat is the max stress theory?</h3>
The most shear strain concept states that the failure or yielding of a ductile fabric will arise whilst the most shear strain of the fabric equals or exceeds the shear strain fee at yield factor withinside the uniaxial tensile test.”
Stress states at various critical locations are f= 2.662.
Read more about strain:
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The council from which Sarah can obtain her building certification is;
<u><em>US Green Building Council</em></u>
- We are told that Sarah is an environmental activist because she conducts a lot of programs to advocate for clean and sustainable environment.
Now, there is a program called LEED which is an acronym for <em>Leadership in </em>
<em>Energy and Environmental Design</em> standards that is necessary for those
that want to measure the greenness of buildings.
This <em>LEED</em> program explained above is organized by an organization in
the United States of America (USA) known as US Green Building Council
(USGBC). This program is for everyone who wants to be a certified
environmental activist and thus i t is recommended that Sarah gets her
certification here.
Read more at; brainly.com/question/24611198
Answer:
True
Explanation:
An LED test light is a piece of electronic test equipment used to determine the presence of electricity in a piece of equipment under test, making this statement true.
Answer:
a) specific impulse = 203 s
(b) mass flow rate = 2511 kg/s
(c) throat diameter = 0.774 m
(d) exit diameter = 1.95 m
(e) thrust = 5.3*10^6 N/m^2
(f) thrust at sea level = 15.6*10^6 N
(g) thrust with hydrogen = 5*10^6 N
(h) thrust with stagnation = 5*10^6 N
Explanation:
See the attached file for explanation.