Answer:
we are become black . and we may suffer from many disease . and our face and body become dull .
Answer:
the cerebrum, cerebellum and brainstem. Cerebrum: is the largest part of the brain and is composed of right and left hemispheres. It performs higher functions like interpreting touch, vision and hearing, as well as speech, reasoning, emotions, learning, and fine control of movement.
Explanation:
Since the options have not been given the question is incomplete. The complete question is as follows:
The health care provider is discussing major risk factors for coronary artery disease (CAD) with a client. The most important information for the provider to include would be:
a)History of cigarette smoking and elevated blood pressure
b)Physical inactivity and high serum high-density lipoprotein cholesterol
c)High serum high-density lipoprotein and diabetes
d)Advanced age and low serum total and low-density lipoprotein cholesterol
Answer: a)History of cigarette smoking and elevated blood pressure
Explanation:
CAD is a plaque or clot development in the walls of the arteries that supplies blood to the entire body. Plaque develops due to deposition of cholesterol and other substances in the arteries. This affects the blood flow.
The chemicals in the cigarette smoke develops plaque or clots in the blood vessels or arteries. This affects the blood pressure. Thus the blood pressure get elevated. The chemicals in the smoke causes the blood vessels to get swollen and inflamed. This increases the risk of strokes.
Answer:
18.6x + 3.6
Explanation:
A rocket scientist needs to find the overall thrust of a new rocket design. The rocket has two stages: Stage A and Stage B. Stage A's thrust is defined by the expression 11.2x + 6.4 and Stage B's thrust is defined by the expression 7.4x − 2.9.
Solution:
The rocket thrust is the force that helps in moving the rocket through air and through space. For a multistage rocket, the overall thrust is gotten by summing all the thrust experienced in each of the stages.
Hence the overall thrust for this problem is given by the equation:
Overall thrust = Stage A thrust + stage B thrust
Overall thrust = (11.2x + 6.4) + (7.4x − 2.9)
Overall thrust = 18.6x + 3.6
Show them exactly what you are doing. Let them see the rubric for the report.