The transition time of a diode is 3.6 times the storage time, if the reverse recovery time is 13 nS, what is the storage time in nS?
a.2,32142857
b.None
c.1,96969697
d.2,82608696

Answers

Answer 1

The storage time can be calculated by dividing the reverse recovery time by 3.6.The transition time of a diode is 3.6 times the storage time, b.None if the reverse recovery time is 13 nS.

Storage time = Reverse recovery time / 3.6Given that the reverse recovery time is 13 nS, we can calculate the storage time as follows:Storage time = 13 nS / 3.6 ≈ 3.6111 nSTherefore, the storage time is approximately 3.6111 nS.Since none of the provided answer choices match this value exactly, the correct answer would be (b) None.

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Related Questions

What kind of plan or development of road can be done to avoid traffic?​

Answers

Answer: Breakdown Lanes

Reason: With breakdown lanes when a car needs to stop it can go to the backdown lane and fix its issue.

Under a subsection for geological hazards the buyer is encouraged to obtain an read the booklet

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Answer:

Buyer is encouraged to obtain and read the booklet entitled "The Homeowners Guide to Earthquake Safety." In most cases a questionnaire within the booklet must be completed by Seller and the entire booklet given to the Buyer if the Property was built prior to 1960.

Consider filling a cylinder of compressed argon from a high- pressure supply line as shown below. Before filling, the cylinder contains 10 bar of argon at room temperature. The valve is then opened, exposing the tank to a 50 bar line at room temperature un- til the pressure of the cylinder reaches 50 bar. The valve is then closed. For argon take cP = (5/2)R and the molecular weight to be 40 g mol. You may use the ideal gas model. (a) What is the temperature right after the valve is closed? (b) If the cylinder sits in storage for a long time, how much heat is transferred (in kJ/kg)? (c) What is the pressure of the cylinder when it is shipped (after it was stored for a long time)?

Answers

The initial pressure in the cylinder of 10 bar of argon with \(C_p\) = (5/2)·R

and the added gas at pressure of 50 bar gives the following values.

(a) 400.6 K

(b) 51.184 J

(c) The pressure of the cylinder when it is shipped is 37.194 bar

How can the temperature, heat transferred and pressure be calculated?

(a) Adiabatic compression, we have;

\(\dfrac{p_{1}}{p_{2}} = \mathbf{\left (\dfrac{T_{_{1}}}{T_{2}} \right )^{\dfrac{k}{k-1}}}\)

Where;

\(k = \dfrac{C_p}{C_v} = \mathbf{\dfrac{C_p}{C_p - R}}\)

Therefore;

\(K= \mathbf{\dfrac{\frac{5}{2} \cdot R}{\frac{5}{2} \cdot R - R} }= \dfrac{5}{3}\)

Which gives;

\(\dfrac{10}{50} = \left (\dfrac{298}{T_{2}} \right )^{\dfrac{\frac{5}{3} }{\frac{5}{3} -1}} = \left (\dfrac{298}{T_{2}} \right )^{2.5}\)

\(\dfrac{50}{10} = \mathbf{ \left (\dfrac{T_2}{298.15} \right )^{2.5}}\)

\(ln(5)= 2.5\cdot ln\left (\dfrac{T_2}{298.15} \right )\)

\(T_2 = 298 \times e^{\dfrac{ln(5)}{2.5} } \approx \mathbf{567.29\, K}\)

The temperature

Using an ideal gas model, we have;

\(\dfrac{V_{1}}{V_{2}} = \mathbf{\dfrac{P_{2}\times T_{1}}{T_{2} \times P_1}}\)

Which gives;

\(\dfrac{V_{1}}{V_{2}} = \dfrac{50\times 298}{567.29 \times 10} \approx 2.625\)

V₁ = 2.625·V₂

Volume occupied by the gas in the cylinder after the pressure increases is therefore;

\(V_2 = \dfrac{V_1}{2.625} \approx 0.381 \cdot V_1\)

Volume of gas added is therefore;

\(V =V_1 - \dfrac{V_1}{2.625} = 0.619\cdot V_1\)

Considering a molar volume of gas, we have;

0.040 × 0.619 × 2.5×8.3145×(T₃ - 298) = 0.040 × 0.381 × 2.5×8.3145×(567.29 - T₃)

Solving gives;

T₃ ≈ 400.6 K

For a molar volume of gas cylinder, the temperature just after the valve is closed is T₃ ≈ 400.6 K

(b) If the cylinder sits in the storage for a long time, and heat is conducted out, we have;

The temperature of the cylinder will revert to room temperature of 298 K

The heat transferred is therefore;

0.040 × (2.5 × 8.3145 - 8.3145) ×(400.6 - 298) ≈ 51.184

The heat transferred from the cylinder is 51.184 J

(c) The pressure of the gas in the cylinder is therefore;

\(\dfrac{P_1}{T_1} = \mathbf{\dfrac{P_2}{T_2}}\)

Which gives;

\(P_2= \mathbf{\dfrac{P_1}{T_1} \times T_2}\)

Therefore;

\(P_2= \dfrac{50}{400.6} \times 298 \approx 37.194\)

The pressure of the cylinder when it is shipped is 37.194 bar

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A transformer is to be used to provide power for a computer disk drive that needs 6.4 V (rms) instead of the 120 V (rms) from the wall outlet. The number of turns in the primary is 300, and it delivers 500 mA (the secondary current) at an output voltage of 6.4 V (rms). (a) Should the transformer have more turns in the secondary compared to the primary, or fewer turns

Answers

Answer:

The secondary coil should have fewer turns compared to the primary coil.

Explanation:

\(N_p\) = Number of turns in primary coil = 300

\(N_s\) = Number of turns in secondary

\(V_p\) = Voltage in primary coil = 120 V

\(V_s\) = Voltage in secondary coil = 6.4 V

We have the relation

\(\dfrac{N_p}{N_s}=\dfrac{V_p}{V_s}\\\Rightarrow N_s=\dfrac{N_p}{V_p}\times V_s\\\Rightarrow N_s=\dfrac{300}{120}\times 6.4\\\Rightarrow N_s=16\)

The secondary coil has 16 turns which is less than the turns in the primary coil.

will mark brainliestt

will mark brainliestt

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Answer:

Ok.

Explanation:

This is what true artis.

The steel shaft has a diameter of 40 mm and is fixed at its ends A and B . If it is subjected to the couple determine the maximum shear stress in regions AC and CB of the shaft. G st = 75 GPa.
Q6/

Answers

Answer:

See explanation.

Explanation:

Since no figure was given I solved a problem that was similar to the one you described that I worked in my mechanics of materials class. The method should be very similar for your figure. See attached image for my work.

The steel shaft has a diameter of 40 mm and is fixed at its ends A and B . If it is subjected to the

If it is subjected to the couple determine the maximum shear stress in regions AC and CB of the shaft. G st = 75 GPa. Than the answer will be 52Mpa.

What we need to perform?

We need to perform a two step process to obtain the maximum shear stress on the shaft. For the solid shaft,

P=2×pi×N×T/60 or T=60×p/2×pi×N

Where P=power transmitted by the shaft=50×10³W

N=rotation speed of the shaft in rpm=730rpm

Pi=3.142

T is the twisting moment

By substituting the values for pi, N and P, we get

T=654Nm or 654×10³Nmm

Also, T=pi×rho×d³/16 or rho=16×T/pi×d³

Where rho=maximum shear stress

T = twisting moment=654×10³Nmm

d= diameter of shaft= 40mm

By substituting T, pi and d

Rho=52Mpa

b. For a hollow shaft, the value for rho is unknown

T=pi×rho(do⁴-di⁴/do)/16

Rho=T×16×do/pi×(do⁴-di⁴)

Where

T= twisting moment=654×10³Nmm gotten above

do=outside shaft diawter=40mm

di= inside shaft diameter =30mm

Pi=3.142

Substituting values for pi, do, di and T.

Rho=76Mpa

Therefore, If it is subjected to the couple determine the maximum shear stress in regions AC and CB of the shaft. G st = 75 GPa. Than the answer will be 52Mpa.

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In the air with the antiskid armed, current cannot flow to the antiskid control box becauseA. landing gear squat switch is open.B. landing gear down and lock switch is open.C. landing gear antiskid valves are open.

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When the antiskid system is armed during flight, it is designed to prevent skidding of the aircraft's wheels during landing. However, in this state, current cannot flow to the antiskid control box. The reason for this is because the landing gear squat switch is open.

This switch is located on the main landing gear and is designed to detect when the wheels are on the ground during landing. When the switch is closed, it allows the current to flow to the antiskid control box. However, since the switch is open during flight, the current cannot reach the control box, even if the landing gear antiskid valves are open. Therefore, the landing gear squat switch plays a critical role in ensuring the proper functioning of the antiskid system during landing.

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Discuss types of environmental hazards and impact of the environmental hazards.​

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An environmental hazard is a substance, state or event which has the potential to threaten the surrounding natural environment and/or adversely affect human's health. This term incorporates topics like pollution, natural disasters and human-made hazards. Health studies investigate the human health effects of exposure to environmental hazards ranging from chemical pollutants to natural, technological or terrorist disasters. The environment in which we live can be considered as having three fundamental sets of components, physical, chemical, biological. Associations between an exposure and an adverse health effect do not, on their own, prove that the former is the cause of the latter. Many other non-causal associations could explain the findings. Physical hazards involve environmental hazards that can cause harm with or without contact. Examples are earthquakes, electromagnetic fields, floods, light pollution, noise pollution, vibration, x-rays etc. Radioactivity is associated with an exposure dependent risk of some cancers notably leukaemia. The scientific evidence of adverse health effects from general environmental exposure to these fields is "not proven". If there are adverse effects yet to be proven, the risk is probably likely to be small. Chemical substances cause significant damage to the environment. Tobacco smoke is the single biggest known airborne chemical risk to health, whether measured in terms of death rates or ill-health. To a much lesser degree of risk, these adverse effects apply to non-smokers exposed passively to sidestream tobacco smoke. Health effects of concern are asthma, bronchitis, lung cancer and similar lung diseases, and there is good evidence relating an increased risk of symptoms of these diseases with increasing concentration of Sulphur dioxide, ozone and other pollutants. Biohazards generally fall into two broad categories: those which produce adverse health effects through infection (microorganisms, viruses or toxins) and those which produce adverse effects in non-infective (allergic) ways.

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Write ARM assembly code to reverse the bits in a register. Use as few instructions as possible. Assume to register of interest is R3.

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Sure, here's the ARM assembly code to reverse the bits in a register:

MOV R0, #32       ; initialize counter to 32
REV R3, R3        ; reverse the bits in R3
loop:
LSRS R1, R3, #31  ; get the rightmost bit of R3
ORRS R1, R1, R1, LSL #31 ; move it to the leftmost position
LSLS R3, R3, #1   ; shift R3 left by one bit
ORRS R3, R3, R1   ; set the rightmost bit of R3 to the value of R1
SUBS R0, R0, #1   ; decrement counter
BNE loop          ; repeat until all 32 bits have been reversed

This code uses the REV instruction to quickly reverse the bits in the register, and then loops through each bit using shifts, masks, and logical operations to put them back in the reverse order. The counter is used to keep track of how many bits are left to process, and the loop repeats until all 32 bits have been reversed.

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What signal propagation phenomena causes the diffusion, or the reflection in multiple different directions, of a signal?

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In the radio communication system, multipath is the propagation phenomenon that causes diffusion or reflection in multiple different directions of a signal.

Multipath is a propagation mechanism that impacts the propagation of signals in radio communication. Multipath results in the transmission of data to the receiving antenna by two or more paths. Diffusion and reflection are the causes that create multiple paths for the signal to be delivered.

Diffraction occurs when a signal bends around sharp corners; while reflection occurs when a signal impinges on a smooth object. When a signal is received through more than one path because of the diffraction or reflection, it creates phase shifting and interference of the signal.

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: Delivery Execution Knowledge Check Question 1 of 8. When you walk into the station at the end of your route, what should you do?
O Check in with your DSP and being any undeliverable packages back to the Amazon Retum to Station desk
O leave the undeliverable packages with your OSP then go off duty
O You don't have to return to the station at the end of your day
O Sign out of your device and love
Mark for foto up

Question 2 of 8. How do you make sure that you are at the correct address?
O Compare the address on the package label with the address listed in your delivery app
O Compare the address in your delivery app with the physical home address
O Compare the address isted on the package label with the address listed in
O Delivery App, and the physical address listed on the home The delivery app will tell you the correct address
Mark forfollow up

Question 3 of 8 In the Delivery App, where can you find the button to contact the customer?
O In the Map screen
O In the Help menu
O in the linerary
O In the Main Menu

Answers

When you walk into the station at the end of your route, you should option A: check in with your DSP and bring any undeliverable packages back to the Amazon Return to Station desk.

2. To make sure you are at the correct address, you should option A: compare the address on the package label with the physical home address. You can also compare the address listed in your delivery app with the physical address.


3. In the Delivery App, you can find the button to contact the customer in option A:  the Map screen or in the itinerary. It may be labeled "Contact Customer" or something similar.

What is the Delivery Execution Knowledge?

When you finish your delivery route and return to the station, it is important to check in with your DSP (Delivery Service Provider) and return any undeliverable packages to the Amazon Return to Station desk. This helps to ensure that the packages are properly processed and that the delivery information is accurately recorded.

Therefore, To make sure you are at the correct address, you should compare the address on the package label with the physical home address.

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The acceleration function of an object doing curvilinear motion is a = {(-0.2)i+2j+1.5k) m/s², where t is in s. If its initial velocity vo 8i m/s, and initial position is at the origin, determine the magnitude of its velocity when t = 3 s.​

Answers

Asnwer:
To solve this problem, we need to integrate the acceleration function to obtain the velocity function, and then evaluate the magnitude of the velocity at t = 3 s.

The velocity function can be obtained by integrating the acceleration function as follows:

v(t) = ∫a(t)dt

v(t) = ∫((-0.2)i+2j+1.5k)dt

v(t) = (-0.2t)i+(2t)j+(1.5t)k + C

where C is a constant of integration. To determine the value of C, we can use the initial velocity, which is given as vo = 8i m/s when t = 0 s:

v(0) = (-0.2(0))i+(2(0))j+(1.5(0))k + C = 8i

C = 8i

Therefore, the velocity function is:

v(t) = (-0.2t)i+(2t)j+(1.5t)k + 8i

Now, to determine the magnitude of the velocity at t = 3 s, we can simply evaluate the velocity function at t = 3 s and compute its magnitude:

v(3) = (-0.2(3))i+(2(3))j+(1.5(3))k + 8i

v(3) = (-0.6)i+6j+4.5k + 8i

v(3) = 7.4i+6j+4.5k

|v(3)| = sqrt((7.4)^2 + 6^2 + (4.5)^2)

|v(3)| = sqrt(102.41 + 36 + 20.25)

|v(3)| = sqrt(158.66)

|v(3)| ≈ 12.6 m/s (rounded to one decimal place)

Therefore, the magnitude of the velocity when t = 3 s is approximately 12.6 m/s.

Answer:

the magnitude of the velocity when t = 3 s is 10.54 m/s.

Explanation:

To solve this problem, we can use the following kinematic equation that relates velocity, acceleration, and time:

v = vo + at

where:

v = final velocity

vo = initial velocity

a = acceleration

t = time

First, we need to find the velocity of the object at time t = 3 s. To do this, we can substitute the given values into the kinematic equation and solve for v:

v = vo + at

v = 8i + (-0.2i+2j+1.5k) x 3

v = 8i - 0.6i + 6j + 4.5k

v = 7.4i + 6j + 4.5k

The magnitude of the velocity is given by:

|v| = sqrt(vx^2 + vy^2 + vz^2)

where:

vx, vy, vz = the x, y, and z components of the velocity vector

Substituting the values from above, we get:

|v| = sqrt((7.4)^2 + 6^2 + (4.5)^2)

|v| = sqrt(54.81 + 36 + 20.25)

|v| = sqrt(111.06)

|v| = 10.54 m/s (approx)

Q1: You have to select an idea developing an application like web/mobile or industrial, it should be based on innovative idea, not just a simple CRUD application. After selecting the idea do the following: 1) How your project will be helpful and what problem this project addresses. (10-Marks) 2) Write down the requirements. (10Marks) 3) List the functional and non-functional requirements of your project. (10marks) 4) Which process model you will follow for this project and why? (10marks) 5) Draw the Level 0, and level 1 DFD of your application. (20marks)

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Answer:

Creating an app is both an expression of our self and a reflection of what we see is missing in the world. We find ourselves digging deep into who we are, what we would enjoy working on, and what needs still need to be fulfilled. Generating an app idea for the first time can be extremely daunting. Especially with an endless amount of possibilities such as building a church app.

The uncertainty has always spawned a certain fear inside creators. The fear of creating something no one will enjoy. Spending hundreds of dollars and hours building something which might not bring back any real tangible results. The fear of losing our investment to a poor concept is daunting but not random. But simple app ideas are actually pretty easy to come by.

Great app idea generation is not a gift given to a selected few, instead, it is a process by which any of us are able to carefully explore step by step methods to find our own solution to any problem. Whether you are a seasoned creator or a novice, we have provided a few recommendations to challenge and aid you as you create your next masterpiece.

if I am right then make me brainliest

Sally made a diagram to show one way that Earth’s systems interact near a volcano.

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We won’t be able to do it cuz we can’t draw on this app

3. 21 A three-phase load draws 120 kW at a power factor of 0. 85 lagging from a 40-V bus. In parallel with this load is a three-phase capacitor bank that is rated 50 VAR. Find (a) the total line current and (b) the resultant power factor

Answers

To calculate the total line current, we can use the formula:

I = P / (sqrt(3) x V x pf)

where I is the line current, P is the power, V is the voltage, and pf is the power factor.

Substituting the given values, we get:

I = 120,000 / (sqrt(3) x 40 x 0.85) = 1,389 A

To find the resultant power factor, we can use the formula:

pf = (P1 + P2) / (sqrt(3) x V x I)

where P1 is the power of the load, P2 is the reactive power of the capacitor bank, and the rest of the variables are as defined above.

Substituting the given values, we get:

pf = (120,000 + 50) / (sqrt(3) x 40 x 1,389) = 0.872 lagging

Therefore, the total line current is 1,389 A and the resultant power factor is 0.872 lagging.

Consider a system consisting of the cascade of two LTI systems with frequency responses 2 e-jw Н (e'») 1e-jw and 1 H2(eu) 1 e-jw e-2w+ (a) Find the difference equation describing the overall system (b) Determine the impulse response of the overall system

Answers

The difference equation of the overall system can be found by taking the inverse Z-transform of the product of the two transfer functions and the impulse response by taking the inverse Z-transform of the resulting d.e.

The overall system can be represented by H1(e^jw)H2(e^jw), where H1(e^jw) is the frequency response of the first LTI system and H2(e^jw) is the frequency response of the second LTI system. The difference equation describing the overall system can be obtained by taking the inverse Z-transform of the product of H1(e^jw) and H2(e^jw).

Thus, the difference equation of the overall system is given by y[n] - y[n-1] + 2x[n] - 2x[n-1] + x[n-2] = 0, where y[n] and x[n] are the output and input signals of the overall system, respectively.

To determine the impulse response of the overall system, we can set x[n] = δ[n], where δ[n] is the unit impulse function. Thus, the difference equation reduces to y[n] - y[n-1] + 2δ[n] - 2δ[n-1] + δ[n-2] = 0.

Taking the Z-transform of this equation, we get Y(z)(1 - z^-1) + 2(1 - z^-1) - 2z^-1 + z^-2 = 0. Rearranging and solving for Y(z), we obtain Y(z) = (2 - z^-1)/(1 - z^-1 + z^-2).

Finally, taking the inverse Z-transform of Y(z), we obtain the impulse response of the overall system as h[n] = 2^n u[n] - (2^n-1)u[n-1], where u[n] is the unit step function.

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A comparison of parking fee changed at 4 randomly selected parking areas were 12 15 17 and 20 pesos per car find the mean the variance of the parking fees

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The calculated mean value is 16. The sum of all values divided by the total number of values determines the mean (also known as the arithmetic mean, which differs from the geometric mean) of a dataset.

The term "average" is frequently used to describe this measure of central tendency. By dividing the sum of the given numbers by the entire number of numbers, the mean—the average of the given numbers—is determined. Mean is equal to (Sum of All Observations/Total Observations).

Mean=12+15+17+20/4

=16

Special road signage designate 10-cent zones. At the beginning and finish of the zone, there are signs. There is one space available for as long as three or four hours each day. Only specific hours of the day are subject to the 10 cent rate. There may be a Blue Zone in locations where paid parking is not (yet) in effect.

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Calculate the maximum value of shear flow, , in the web at a section 1m from the free end of the beam.

Answers

Answer:

See explanation

Explanation:

Since no figure was given, I'll explain how to do this problem theoretically. The formula for shear flow is \(q=\frac{VQ}{I}\) where V is the shear force, Q is the moment of area (more on this later), and I is the moment of inertia.

The first step to solve this problem is to find the resultant internal forces of the beam. This can be done in several ways, but the easiest is to solve the beam statically and draw a shear diagram to determine the maximum shear force V.

The second step to solving this problem is to determine the location of the neutral axis of the cross section if it is not given. The formula for the neutral axis is  \(NA = \frac{\sum y*A}{\sum A}\). The y in this equation represents the middle of the small shapes that the web is divided into. An I-beam can be thought of as 3 rectangles, while a T-beam can be thought of as 2. The A in this formula represents the area of each of the rectangles (an I-beam will have 3 of these and a T-beam will have 2).

The third step for this problem is to find the moment of inertia. There are several formulas for moment of inertia depending on the shape of the cross section. I-beam's and T-beams both can be thought of as multiple rectangles, so they have the same base formula of \(I=\frac{1}{12}bh^3\) where b is the base of the rectangles and h is the height. For I-beams, the easiest way to calculate moment of inertia is to think of the entire cross section as a big rectangle that had two smaller rectangles cut out of it. The formula for this moment of inertia becomes \(I=\frac{1}{12} b_{big}h^{3} _{big}-\frac{1}{6}b_{small}h^{3}_{small}\). Note that this form of moment of inertia already takes into account subtracting 2 small rectangles. For T-beams, this approach will not work, so the parallel axis theorem must be used. The moment of inertia for the T-beam becomes \(I=\frac{1}{12}b_{1} h^{3}_{1} +b_{1}h_{1}dy_{1}^{2} +\frac{1}{12}b_{2} h^{3}_{2} +b_{2}h_{2}dy_{2}^{2}\) where the terms with the subscript 1 represent the first rectangle and the terms with the subscript 2 represent the second rectangle. The dy terms represent the distance from the center of that specific rectangle to the neutral axis.

The fourth step for this problem is to find Q. The formula to find Q is \(Q=\sum y'A'\) where y' represents the distance from the neutral axis to the center of the "wanted" point and A' is the area of the rectangle that has the wanted point at its center. (This would be the area above or below the thickness (t) if you were solving for maximum shear \(\tau=\frac{VQ}{It}\)).

The last step for this problem is to substitute the found values into the formula for shear flow \(q=\frac{VQ}{I}\). V came from step 1, Q came from step 4, and I came from step 3.

Nêu các kí hiệu và kích thước của các
khổ giấy chính ?

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Answer:

sorry I can't understand your language

Explanation:

The Rule That Packets Not Originating From Inside Your LAN Should Not Be Forwarded Relates To ___________. Question 31 Options: 1) Servers 2) Workstations 3)

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The Rule That Packets Not Originating From Inside Your LAN Should Not Be Forwarded Relates to routers

What is meant by routers ?

In order to transfer data between two or more packet-switched computer networks, a router—either real or virtual—is used.. The Internet Protocol address (IP address) of the destination is examined by a router, which then determines the optimal path for the data packet to take to get there.

According to the various application categories, there are five different types of routers available. They include VPN routers, core routers, edge routers, wireless routers, and wired routers. The aforementioned fundamental details can be used to aid in making the best router selection possible.

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The Aluminum Electrical Conductor Handbook lists a dc resistance of 0. 01558 ohm per 1000 ft at 20°C and a 60-Hz resistance of 0. 0956 ohm per mile at 50°C for the all-aluminum Marigold conductor, which has 61 strands and whose size is 1113 kcmil. Assuming an increase in resistance of 2% for spiraling, calculate and verify the dc resistance. Then calculate the dc resistance at 50°C, and determine the percentage increase due to skin effect. The resistivity of the conductor at 20°C is 17. 00 Ω-cmil/ft

Answers

Where the above conditions exists, the DC resistance at 50°C with skin effect is 77.2% higher than the DC resistance at 50°C without skin effect.

What is the explanation for the above?

To calculate the DC resistance at 20°C, we can use the given dc resistance per 1000 ft:

DC resistance per ft = (0.01558 ohm / 1000 ft) * (1113 kcmil / 1000 cmil)

= 0.01735 ohm/ft

Next, we need to account for the 2% increase in resistance due to spiraling:

Resistance increase due to spiraling = 2% * 0.01735 ohm/ft

= 0.000347 ohm/ft

Therefore, the total DC resistance at 20°C is:

DC resistance at 20°C = 0.01735 ohm/ft + 0.000347 ohm/ft

= 0.017697 ohm/ft

To calculate the DC resistance at 50°C, we need to use the temperature coefficient of resistance for aluminum, which is 0.00403/°C. The resistance at 50°C can be found using the following formula:

R(50) = R(20) [1 + α(50 - 20)]

where R(20) is the DC resistance at 20°C and

α is the temperature coefficient of resistance for aluminum.

R(50) = 0.017697 ohm/ft [1 + 0.00403/°C * (50°C - 20°C)] = 0.019371 ohm/ft

The percentage increase due to skin effect can be calculated using the following formula:

% increase due to skin effect = 100 * (R(50) - R(dc)) / R(dc)

where R(dc) is the DC resistance at 50°C without skin effect.

R(dc) = 0.0956 ohm/mile * 5280 ft/mile / 61 strands

= 0.08503475442 ohm/ft

% increase due to skin effect = 100 * (0.019371 ohm/ft - 0.08503475442 ohm/ft) / 0.08503475442 ohm/ft

= 77.2%

Therefore, the DC resistance at 50°C with skin effect is 77.2% higher than the DC resistance at 50°C without skin effect.

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The logarithmic mean temperature difference ∆Tln is an exact representation of the average temperature difference between the fluid and the surface for the entire tube.

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The logarithmic mean temperature difference is a useful parameter in heat transfer analysis as it accounts for the non-uniformity of temperature distribution and provides an exact representation of the average temperature difference for the entire tube.

The logarithmic mean temperature difference (∆Tln) is a widely used parameter in heat transfer analysis. It represents the average temperature difference between the fluids and the surface of the entire tube. It is an exact representation of the temperature difference because it takes into account the non-uniformity of temperature distribution over the length of the tube. This non-uniformity is caused by the flow of fluids and the heat transfer rate, which vary with distance along the tube. The logarithmic mean temperature difference allows for a more accurate calculation of the heat transfer rate compared to a simple average temperature difference.

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Can someone help with this please?

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Answer:

with what

Explanation:

Which of the following is considered an occupancy area and must be included in residential load calculations?

Answers

In residential load calculations, a bedroom is considered an occupancy area and must be included.

What is a Bedroom?

It is a designated living space within a residential dwelling where individuals sleep and spend extended periods. Garages, storage sheds, and backyard patios are typically not considered occupancy areas for load calculations, as they are not commonly used as living spaces.

However, it's important to note that specific building codes and regulations may vary, so it's advisable to consult local guidelines for accurate information pertaining to your region.

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The Complete Question

Which of the following is considered an occupancy area and must be included in residential load calculations?A garageA storage shedA backyard patioA bedroom

Pick one product an engineer would build the basic knowledge of engineering(6that would be used and the product development and express a conclusion doesn’t have to be more than 100 words.

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Aerospace engineers design, analyze, model, simulate, and test aircraft, spacecraft, satellites, missiles, and rockets. Aerospace technology also extends to many other applications of objects moving within gases or liquids. Examples are golf balls, high-speed trains, hydrofoil ships, or tall buildings in the wind. As an aerospace engineer, you might work on the Orion space mission, which plans on putting astronauts on mars by 2020. Or, you might be involved in developing a new generation of space telescopes, the source of some of our most significant cosmological discoveries. But outer space is just one of many realms to explore as an aerospace engineer. You might develop commercial airliners, military jets, or helicopters for our airways. And getting even more down-to-earth, you could design the latest ground and sea transportation, including high-speed trains, racing cars, or deep-sea vessels that explore life at the bottom of the ocean.

For binary flash distillation, we discussed in class that there are 8 variables (F, ZA, V, ya, L, XA, P and T) and 4 equations derived from VLE and mass balances. Thus, we typically require 4 of these variables to be given so that we can obtain a unique solution to the problem. Let's say, your manager tells you that he has a feed mixture with 2 components (given F, za) and he requires you to come up with a flash column that can produce a certain desired amount of Vapor product (thus V, ya are specified). Identity of both components is known and all VLE data has been provided to you. Has the manager given you enough data? If yes, give a step-by-step description of how would you go about designing the flash column (basically find P and T)? If no, why?

Answers

Answer:

yes

Explanation:

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The spread on a proposed road paved with smooth asphalt and having a 1.0-percent longitudinal slope is limited by local regula- tions to 3.0 m for the sake of au- tomobile safety. The road cross- slope is 2.5%. What is the maximum allow- able discharge on the road if the gutter section is uniform? What is the depth of the flow measured at the curb for this rate of discharge? An alternative design proposes the addition of a gutter de- pression with a width of 1.5 meters and a gutter cross-slope of 4.0%. What is the maximum allowable discharge in the gutter under these conditions? What is the depth of the flow at this rate of discharge? Does the addition of the gutter depression increase or decrease the capacity of the gutter? Why?

Answers

The maximum allowable discharge for the road is 0.225 m³/s with a depth of 3.0 meters. Adding a gutter depression doesn't change the capacity, which remains at 0.18 m³/s with a depth of 3.0 meters.

To calculate the maximum allowable discharge and the depth of flow for the given road conditions, let's follow the steps:

Step 1: Calculate the cross-sectional area of flow for the road without the gutter depression.

The cross-slope of the road is 2.5%, which means for every meter of horizontal distance, there is a rise of 2.5 cm.

Cross-sectional area = road width * road cross-slope

                  = 3.0 m * (2.5/100)

                  = 0.075 m²

Step 2: Calculate the maximum allowable discharge on the road without the gutter depression.

The maximum allowable discharge is limited by the spread, which is 3.0 m.

Maximum allowable discharge = cross-sectional area * spread

                          = 0.075 m² * 3.0 m

                          = 0.225 m³/s

Step 3: Calculate the depth of flow at the curb for this rate of discharge.

To find the depth of flow, we need to divide the discharge by the cross-sectional area.

Depth of flow = Maximum allowable discharge / cross-sectional area

            = 0.225 m³/s / 0.075 m²

            = 3.0 m

Therefore, the depth of flow at the curb for the maximum allowable discharge is 3.0 meters.

Step 4: Calculate the maximum allowable discharge and the depth of flow for the road with the gutter depression.

The gutter depression has a width of 1.5 meters and a cross-slope of 4.0%.

Cross-sectional area of the gutter = gutter width * gutter cross-slope

                                = 1.5 m * (4.0/100)

                                = 0.06 m²

Maximum allowable discharge in the gutter = cross-sectional area of the gutter * spread

                                        = 0.06 m² * 3.0 m

                                        = 0.18 m³/s

Depth of flow in the gutter = Maximum allowable discharge in the gutter / cross-sectional area of the gutter

                          = 0.18 m³/s / 0.06 m²

                          = 3.0 m

The depth of flow in the gutter is also 3.0 meters.

Step 5: Determine the effect of the gutter depression on the capacity of the gutter.

The addition of the gutter depression does not increase or decrease the capacity of the gutter. The capacity remains the same at a maximum allowable discharge of 0.18 m³/s and a depth of flow of 3.0 meters. The purpose of the gutter depression is to provide a channel for efficient water drainage, but it does not affect the overall capacity of the gutter.

To summarize:

- The maximum allowable discharge on the road without the gutter depression is 0.225 m³/s, and the depth of flow at the curb is 3.0 meters.

- The maximum allowable discharge in the gutter with the gutter depression is 0.18 m³/s, and the depth of flow in the gutter is also 3.0 meters.

- The addition of the gutter depression does not affect the capacity of the gutter; it provides efficient drainage without altering the maximum allowable discharge or depth of flow.


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2. Describe how these variables will be affected by the use of flaps.
a. Lift
b. Drag
c. Takeoff airspeed
d. Takeoff distance
e. Wing camber ​

Answers

The flap is used to lift the aircraft in the air as it provides them with balance.

What are flaps?

The flaps' main function is to produce additional pull during decreased airspeed, therefore allowing the aircraft to fly at much low rpm with a reduced chance of crashing.

The flap is used to lift the aircraft in the air as it provides them with balance.

They are used for dragging the aircraft as it provides them with a certain amount of height with increases and lowers it.

The takeoff speed is slowed so relatedly to the flap as the change in the structure for the dynamic effect of the airspeed.

Flap reduces the takeoff distance as a smaller speed is being created, which reduces the feed with the coefficient of lift.

The class have a chamber it provides some hollow stairs through which they can store the good and services also it is sometimes used for oil storage.

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8. What are two ways SpaceX plans to change personal travel?

Answers

Answer:

as all the people should go near stratosphere

I. Convert the following numbers with the indicated bases to decimal:
1. (1O111O)2
2. (1110101.11)2
3. (12121)3
4. (4310)5
5. (50)7
6. (198)12

Answers

I think it will be 2 ( 1110101.11)

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