It is not a practical proposition to take direct measurements in nanoscale, but we can estimate variations in position and momentum of particles by a)-Scanning Electron Microscopes b)-Transmission Electron Microscope c)-Heisenberg Uncertainly Principle d)- None of the above

Answers

Answer 1

Answer:

Answer is c Heisenberg's uncertainty principle

Explanation:

According to Heisenberg's uncertainty principle there is always an inherent uncertainty in measuring the position and momentum of a particle simultaneously.

Mathematically

[tex]\Delta x\times \Delta \overrightarrow{p}\geq \frac{h}{4\pi }[/tex]

here 'h' is planck's constant


Related Questions

What are the air-standard assumptions?

Answers

Answer:

The air-standard assumptions are:

The working fluid is air assumed to be perfect and it behave as an ideal gas .All process are internally reversible.The cycle is modeled as closed cycle with air cooled in the chiller heat exchanger and then re-circulated to the compressor. To avoid the complications, the combustion container are replaced by combustion heat exchanger .

________is defined to be the probability that a failed component or system will be restored to a repaired specified condition within a period of time when maintenance is performed in accordance with prescribed procedures

Answers

Answer:

Repairable component

Explanation:

Repairable component is defined to be the probability that a failed component or system will be restored to a repaired specified condition within a period of time when maintenance is performed in accordance with prescribed procedures.

________is defined to be the probability that a failed component or system will be restored to a repaired specified condition within a period of time when maintenance is performed in accordance with prescribed procedures

Repairable component

What is pre-flush and post flush in petroleum engineering?

Answers

Answer:

Pre-Flush:

It is also known as In-line Equalization. In this stage of flow equalization, all the flow passes through the equalization basin. It helps in reduction of fluctuation in pollutants concentration and flow rate and helps to control short term surges with the use of basin.

Post-Flush:

Another name for this stage is Off-line Equalization. In this stage, only overflow above a predetermined standard is diverted into the basin. It helps in reducing the fluctuations in loading by a considerable amount and helps to reduce the pumping requirement. It is basically used to capture "first flush" from combined collection systems.

Answer:

Answer:

Pre-Flush:

It is also known as In-line Equalization. In this stage of flow equalization, all the flow passes through the equalization basin. It helps in reduction of fluctuation in pollutants concentration and flow rate and helps to control short term surges with the use of basin.

Post-Flush:

Another name for this stage is Off-line Equalization. In this stage, only overflow above a predetermined standard is diverted into the basin. It helps in reducing the fluctuations in loading by a considerable amount and helps to reduce the pumping requirement. It is basically used to capture "first flush" from combined collection systems.

Explanation:

A water pipe with a 5 cm inner diameter is designed for to have a flow rate of 75 Umin. What is the entrance length for this pipe (in cm)?

Answers

Answer:

121.20 cm

Explanation:

Given data in question

inner dia = 5 cm

flow rate = 75  umin = 1.25 ×10³ cm³/sec

Solution

First we calculate Re by this formula

Re= [tex]\frac{V × D}{v)}[/tex]  = [tex]\frac{Q × D}{π/4 × D²× v)}[/tex]

Re= [tex]\frac{4Q }{π × D× v)}[/tex]

here we know Q is flow rate and D is dia of pipe and v is kinematic viscosity that is 1.14 × [tex]10^{-2}[/tex] cm ² / sec

so Re= [tex]\frac{4Q }{π × D× v)}[/tex]

Re = [tex]\frac{4×1.25× 10³ }{π × 5 × 1.14 × 10^{-2}  )}[/tex]

So Re will be 27936 that is greater than 4000 thats why it is turbulent flow

and we know [tex]\frac{Length}{dia)}[/tex] ≡ 4.4 [tex]Re^{1/6}[/tex]

so [tex]\frac{Length}{dia)}[/tex] ≡ 24.24

length will be 121.20 cm

Three point bending is better than tensile for evaluating the strength of ceramics. a)-True b)- False

Answers

Answer:

a)-True

Explanation:

Three point bending is better than tensile for evaluating the strength of ceramics. It is got a positive benefit to tensile for evaluating the strength of ceramics.

Water flows in a pipe of diameter 0.5 m. The dianeter of the to 1,0 m. A U-tube manometer is of the enlargement with joining ercury levels 5 mm. Determine the flow rate as well as the pressure 3 Water pipe suddenly enlarges connected to either side pipes which contain water. The difference in m head loss as a result of the enlargement.

Answers

Answer:

Q = 0.943[tex]m^{3}/s[/tex]

[tex]h_{L}[/tex] = 0.6605 m

Explanation:

Given :

Diameter, d₁ = 0.5 m

Area, A₁ = [tex]\frac{\pi }{4}\times 0.5^{2}[/tex]

             = 0.19625 [tex]m^{2}[/tex]

Enlargement diameter, d₂ = 1 m

Enlargement Area, A₂ = [tex]\frac{\pi }{4}\times 1^{2}[/tex]

             = 0.785 [tex]m^{2}[/tex]

Manometric difference, h = 35 mm

                                          =35 X [tex]10^{-3}[/tex] m

From manometer , we get

[tex]P_{1}+\rho _{w}.g.z_{1}+\rho _{m}.g.h=P_{2}+\rho _{w}.g.(z_{1}+h)[/tex]

[tex]P_{1}-P_{2}=(\rho _{w}-\rho _{m}).g.h[/tex]

[tex]\frac{P_{1}-P_{2}}{\rho _{w}.g}=(1-\frac{\rho _{m}}{\rho _{w}})\times h[/tex]

                                                = [tex](1-13.6)\times 35\times 10^{-3}[/tex]

                                                = -0.441

Now from newtons first law,

[tex]\frac{P_{1}-P_{2}}{\rho _{w}.g}=\frac{V_{2}^{2}-V_{1}V_{2}}{g}[/tex]

-0.441 = [tex]\frac{Q^{2}}{9.81}\times (\frac{1}{A_{2}^{2}}-\frac{1}{A_{1}A_{2}})[/tex]

-0.441 = [tex]\frac{Q^{2}}{9.81}\times (\frac{1}{0.785^{2}}-\frac{1}{(0.19625\times 0.785)^{2}})[/tex]

Therefore. Q = 0.943 [tex]m^{3} /s[/tex]

Now V₁ = [tex]\frac{Q}{A_{1}}[/tex]

            = [tex]\frac{0.943}{0.19625}[/tex]

            = 4.80 m/s

       V₂ =  [tex]\frac{Q}{A_{2}}[/tex]

            = [tex]\frac{0.943}{0.785}[/tex]

            = 1.20 m/s

Therefore, heat loss due to sudden enlargement is given by

  [tex]h_{L}=\frac{(V_{1}-V_{2})^{2}}{2g}[/tex]

[tex]h_{L}=\frac{(4.80-1.20)^{2}}{2\times 9.81}[/tex]

               = 0.6605 m

A 5Kw solar system may produce enough energy to power your home. a)-True b)- False

Answers

Answer: True

Explanation:

Yes, it is true that 5 Kw solar system may produce enough energy to power your home as, on an average good quality of 5 KW solar system can produced 22 units per day enough to power all home appliances. As, a 5 KW solar system produced energy is basically depends on the three main factor that are:

Quality of the solar panel system.Location from where the solar system generated its energy.And also on the positioning of the solar system.

The temperature in a pressure cooker is 130 degree C while the water is boiling. Determine the pressure inside the cooker.

Answers

If water is boiling at 130 degrees Celsius inside a pressure cooker, the pressure is approximately 2.7 atmospheres

To determine the pressure inside a pressure cooker where water is boiling at 130 degrees Celsius, we use the properties of water and its boiling point at various pressures.

For water, the pressure at which the boiling point is elevated to 130 degrees Celsius can be found using steam tables.

At 130 degrees Celsius, the saturation pressure of water is approximately 2.7 atmospheres (atm). This is equivalent to :

= 2.7 x 101.325 kPa

= 273.5775 kPa, or about 2.7 bar (since 1 bar = 100 kPa)

Heat in the amount of 100 KJ is transferred directly from a hot reservoir at 1200 K to a cold reservoir at 600K.Calculate the entropy change of the two reservoirs and determine if the increase of entropy principle is satisfied.

Answers

Answer:

0.0833 k J/k

Explanation:

Given data in question

total amount of heat transfedded (Q) = 100 KJ

hot reservoir temperature R(h) = 1200 K

cold reservoir temperature R(c) = 600 k

Solution

we will apply here change of entropy (Δs) formula

Δs = [tex]\frac{Q}{R(h)}+\frac{Q}{R(c)}[/tex]

Δs = [tex]\frac{-100}{1200}+\frac{100}{600)}[/tex]

Δs = [tex]\frac{1}{12}[/tex]

Δs = 0.0833 K J/k

this change of entropy Δs is positive so we can say it is feasible and

increase of entropy principle is satisfied

Answer:

0.0837 kJ/K

Explanation:

Given:

Temperature of the cold reservoir T,cold = 600 K

Temperature of the hot reservoir T,hot= 1200 K

Heat transferred , Q=100 kJ

Now the entropy change for the cold reservoir

[tex]\bigtriangleup S,cold=-\frac{Q}{T,cold}[/tex]

[tex]\bigtriangleup S,cold=-\frac{-100}{600}[/tex]

[tex]\bigtriangleup S,cold=0.1667 kJ/K[/tex]

Now the entropy change for the cold reservoir

[tex]\bigtriangleup S,hot=-\frac{Q}{T,hot}[/tex]

[tex]\bigtriangleup S,hot=-\frac{100}{600}[/tex]

[tex]\bigtriangleup S,hot=-0.0833 kJ/K[/tex]

Therefore, the total entropy change for the two reservoir is

[tex]\bigtriangleup S=\bigtriangleup S,hot +\bigtriangleup S,cold[/tex]

thus,

ΔS=0.1667-0.0833

ΔS=0.0833 kJ/K

Since, the change of entropy is positive thus we can say it is possible and

increase of entropy principle is satisfied

If a host system is 80% efficient, the minimum horsepower rating of the motor should be ? if the hoist is to provide 20,000 ft-lb/s. a) 45.45hp b) 23,530hp c) 36.36hp d) 42.78hp

Answers

Answer:

answer is option A i.e.45.45 hp

Explanation:

Given data:

load =20000 ft lb/s

efficiency = 80%

we know that

1 hp = 550 ft lb/s

minimum horsepower rating can be obtained by using following formula

minimum horse power rating = [tex]\frac{load}{efficiency * 1 horse power} \\[/tex]

                                                = [tex]\frac{20000}{0.8*550} = 45.45 hp[/tex]

What is a substitutional solid solution? And what factors favor the formation of a substitu- tional solid solution?

Answers

Answer:

A substitutional solid solution is a kind of alloying process used to improve or strengthen a purer metal by alloying it. this process works out by adding atoms of an alloy element to the atoms of the crystal lattice of the parent or base element, thus forming a substitutional solid solution. This process generates local non uniformity in the lattice due to the presence or mixing of an alloy element with the base element which impedes the plastic deformation.

Factors that favor the formation of substitutional solid solution are:

Alloying beyond the solubility limitChemical affinity of the elementsRelative atomic size of the particlesCrystal structure of the elementsValence

Answer:

Substitutional solids solution are formed when there is change in position of atom named as A in lattice by some other atoms of different atoms named as B.

Explanation:

Substitutional solids solution are formed when there is change in position of atom named as A in lattice by some other atoms of different atoms named as B.

Strengthening of this solution occurs when solute atom is lager than solvent atom so that it can replace its position

factor affect the extent of solid solution is

1) Relative atomic size

2) crystal structure

3) chemical affinity

4) valency

A fluid with a relative density of 0.9 flows in a pipe which is 12 m long and lies at an angle of 60° to the horizontal At the top, the pipe has a diameter of 30 mm and a pressure gauge indicates a pressure of 860 kPa. At the bottom the diameter is 85 mm and a pressure gauge reading is 1 MPa. Assume the losses are negligible and determine the flov rate. Does the flow direction matter?

Answers

Answer:

[tex]Q=7.3\times 10^{-3} m^3/s[/tex]

Explanation:

Given that

At top[tex]d_2=30 mm,P_2=860 KPa ,P_1=1000 KPa,d_1=85 mm[/tex]

[tex]\rho =900\dfrac{Kg}{m^3}[/tex]

We know that

[tex]\dfrac{P_1}{\rho g}+\dfrac{V_1^2}{2g}+Z_1=\dfrac{P_2}{\rho g}+\dfrac{V_2^2}{2g}+Z_2[/tex]

[tex]A_1V_1=A_2V_2[/tex]

[tex]\frac{V_1}{V_2}=\left(\dfrac{d_2}{d_1}\right)^2[/tex]

[tex]\frac{V_1}{V_2}=\left(\dfrac{30}{85}\right)^2[/tex]

[tex]V_2=8.02V_1[/tex]

[tex]Z_2=12 sin60^{\circ}[/tex]

[tex]\dfrac{1000\times 1000}{900\times 9.81}+\dfrac{V_1^2}{2\times 9.81}+0=\dfrac{860\times 1000}{900\times 9.81 }+\dfrac{V_2^2}{2\times 9.81}+12 sin60^{\circ}[/tex]

So [tex]V_1=1.30[/tex]m/s

We know that flow rate Q=AV

[tex]Q=A_1V_1[/tex]

By putting the values

[tex]A_1=\dfrac{\pi}{4}d^2[/tex]

[tex]Q=7.3\times 10^{-3} m^3/s[/tex]

To find the flow rate we do not need the direction of flow,because we are just doing balancing of energy at inlet and at the exits of pipe.

Convert 25 mm into in.

Answers

Answer:

25 mm = 0.984252 inches

Explanation:

Millimeter and inches are both units of distance. The conversion of millimeter into inches is shown below:

1 mm = 1/25.4 inches

From the question, we have to convert 25 mm into inches

Thus,

25 mm = (1/25.4)*25 inches

So,

[tex]25 mm=\frac{25}{25.4} inches[/tex]

Thus, solving we get:

25 mm = 0.984252 inches

Fluids at rest possess no flow energy. a)- True b)- False

Answers

Answer:

True.

Explanation:

According the engineering flow they don not possess flow energy when they are in rest.

When they are in motion they show a translation energy.

The features if fluids may be different according the variables of pressure and temperature.

An unknown gas (k=1.4, c v= 0.716 kJ/kg.K, c_p=1 kJ/kg.K, R = 0287 kJ/kg K) is trapped in a 1 m^3 piston-cylinder device at 1000 KPa and 1000 K. It then undergoes an isothermal (constant-temp) process in which 696 kJ of boundary work is delivered (positive work transfer). Determine the heat transfer. (Use the PG model).

Answers

Answer:

So heat transfer is 696 kJ

Explanation:

Given:

K = 1.4

[tex]C_{v}[/tex] = 0.716 kJ/kg

[tex]C_{p}[/tex] = 1 kJ/kg

R = 0.287 kJ/kg

V = 1 [tex]m^{3}[/tex]

P = 1000 kPa

T = 1000 K

Work delivered, δW = 696 kJ

It is isothermal process, so the initial and final temperature are same, that is T₁ = T₂ and the internal energy is zero (dU =0)

Therefore from 1st law of thermodynamcis,

δQ = dU + δW

     = 0 + 696

     = 696 kJ

So heat transfer is 696 kJ

What are beats? Determine the terms decibel and octave.

Answers

Answer:

Explained below

Explanation:

Beats are interference pattern between two sounds of slightly different frequencies perceived as periodic vibration in volume whose rate is difference of the two.

Both octave and decibel are the terms of measurement.

Octave(In electronics) is a logarithmic unit for ratio between frequencies,with one octave corresponding to doubling of frequency. For example frequency one octave is from 40 Hz to 80 Hz.

Whereas decibel is a unit of sound intensity. It is one-tenth of A bel. In electronics it is used measure power level of an electrical signal by comparing it with given level of logarithmic scale.

In a nuclear reactor, more fuel is burned than is consumed. a)-True b)- False

Answers

Answer:

true

Explanation:

yes, it is true more fuel is burned than is consumed.

nuclear reactor generate electricity from nuclear fission and while nuclear fission  nucleus splits into small parts to generate energy.

these energies can be used for my purposes mainly it is used for power generation.

we can also say that  in nuclear reactor  more fuel is consumed because of metal acting as a fissionable material.

A wind turbine system has the following specifications: Diameter:45 m Rated power 700 kW at the wind speed of 12 m/s Turbine speed 1500 rpm Determine the swept area of the wind turbine. a)- 1640 m^2 B)- 1690 m^2 c)- 1590 m^2 d)- 1540 m^2

Answers

Answer:

1590 m^2

Explanation:

Given data in this question

Diameter = 45 m

power = 700 kW

wind speed = 12 m/s

turbine speed = 1500 rpm

To find out

swept area of the wind turbine

 

Solution

we know wind turbine is rotate circular form

and diameter is given so by the area of circular swept we will calculate it

we know area =  [tex]\pi /4[/tex] × d²

put the value of d here

area =  [tex]\pi /4[/tex] × 45²

swept area = 1590 m^2

What are the x and y coordinates of the centroid of the area?

Answers

Answer:

[tex]\\X_{C.G}=\frac{\int xdA}{A}\\Y_{C.G}=\frac{\int ydA}{A}[/tex]

Explanation:

The x co-ordinate of the centroid is given by:

[tex]x_{C.G}=\frac{\int xdA}{A}[/tex]

The y co-ordinate of the centroid is given by:

[tex]Y_{C.G}=\frac{\int ydA}{A}[/tex]

where

[tex]x^{}[/tex] is the x co-ordinate of a diffrential area [tex]dA[/tex]

and [tex]y^{}[/tex]  is the x co-ordinate of a diffrential area  [tex]dA[/tex]

See attached figure

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