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3 years ago

What are some basic research topics for writing a research paper for first-year software students?

Engineering

2 answers:

andre [41]3 years ago

6 0

Explanation:

Topics

Introduction of research

research process

(a) planning and other preliminary works

(b) literature review

research process -2

(a) Data collection

(b)dat analysis, presentation and discussion

using research findings or conclusion

(a) designing pilot projects( what works)

FromTheMoon [43]3 years ago

5 0

Writing the Body
Use your outline and prospectus as flexible guides.
Build your essay around points you want to make (i.e., don't let your sources organize your paper) since someone else helped you here’s the a writing body you could use
Integrate your sources into your discussion.
Summarize, analyze, explain, and evaluate published work rather than merely reporting it.

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An intersection had 13 crashes last year. The 4 legs of the intersection had 2-way ADT values of 9671, 2893, 9506, and 2611 vehi

VLD [36.1K]

Answer:

527

Explanation:

Data provided in the question:

Number of crashes per year at the intersection = 13

The 4 legs of the intersection had 2-way ADT values :

9671, 2893, 9506 and 2611 vehicles last year.

Now,

ADT = 9671 + 2893 + 9506 + 2611

= 24,681 vehicles

Rate per Million Entering Vehicles, (RMEV )

= [ ( crashes per year ) ÷ ( Approach ADT per year ) ] × 10⁶

RMEV = [ ( 13 ) ÷ (24,681) ] × 10⁶3

RMEV = 526.721 ≈ 527

8 0

3 years ago

1. Given: R= 25 , E = 100 V<br> Solve for I

Lyrx [107]

Answer:

4 amps

Explanation:

V = I*R

I / V/R

I = 100 / 25

I = 4 amps

5 0

3 years ago

Question 2

ValentinkaMS [17]

Answer:

r h ch y TC GG ch hh h h

No se

Explanation:

No seibibk h j h uh t t t

3 0

2 years ago

A gas turbine has a thermal efficiency of 20% and develops a power output of 8 MW. Determine the fuel consumption rate if heatin

AlexFokin [52]

Answer:

0.8 kilograms of fuel are consumed each second.

Explanation:

As turbines are steady-state devices, the thermal efficiency of a turbine is equal to the percentage of the ratio of the output power to fluid power, that is:

$\eta_{th} = \frac{\dot W}{\dot E} \times 100\,\%$

The fluid power is:

$\dot E = \frac{\dot W}{\eta} \times 100\,\%$

$\dot E = \frac{8\,MW}{20\,\%}\times 100\,\%$

$\dot E = 40\,MW$

Which means that gas turbine consumes 40 megajoules of fluid energy each second, which is heated and pressurized with help of the fuel, whose amount of consumption per second is:

$50\,\frac{MJ}{kg} = \frac{40\,MJ}{m_{fuel}}$