Why can water dissolve some ionic compounds, like NH4Cl, as well as some nonionic compounds, like methanol?

Two surface features that Ganymede appears to have in common with the moon are Craters and Rilles.

Ganymede, the largest moon of Jupiter, shares a couple of surface features in common with Earth's moon. These similarities are:

1. Craters: Both Ganymede and the Moon exhibit numerous impact craters on their surfaces. Craters are formed when meteoroids or other space debris collide with the surface of a celestial body. The presence of craters suggests a history of impacts over time. Both Ganymede and the Moon have craters of varying sizes, ranging from small to large, indicating their geological histories and the impact events they have experienced.

2. Rilles: Rilles are long, narrow depressions or channels on the surface of a celestial body. They can be formed by a variety of processes, including volcanic activity or the collapse of subsurface structures. Ganymede and the Moon both have rilles on their surfaces. For example, the Moon has numerous sinuous rilles, such as the famous Vallis Schröteri (also known as the "Rille of the Serpent"), which are thought to be the result of ancient volcanic activity. Ganymede has a network of grooved terrain that includes linear features resembling rilles, possibly formed by tectonic or volcanic processes.

While Ganymede and the Moon share these surface features, it's worth noting that Ganymede has a more complex geology compared to the Moon. Ganymede has a mix of cratered regions, grooved terrain, and younger, smoother areas, indicating a more diverse geological history influenced by factors such as tectonic activity and subsurface processes, including the presence of a subsurface ocean.

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Answer: layoff

Explanation:

From the information in the question, we can see that Jane is trying to reduce the size of the workforce here through layoff.

Since Joan explains that the termination is temporary, then it's a layoff. If it were to be firing, the termination won't be temporary but permanent as they can't be recalled by the company. But since the employees are discharged temporarily, it's a layoff.

The distance of the ladybug from the center of the platform does affect the angular velocity, and this can be determined by observing the rotational motion of the ladybug.

Angular velocity is the rate at which an object rotates around a specific axis. In the case of the ladybug on a platform, the distance from the center of the platform will indeed impact the angular velocity.

When the ladybug is closer to the center, it has a smaller radius and therefore a smaller distance to travel in a given time, resulting in a higher angular velocity. Conversely, when the ladybug is farther from the center, it has a larger radius and a greater distance to travel, leading to a lower angular velocity.

To determine the effect of the ladybug's distance on the angular velocity, one can observe the rotational motion of the ladybug. By placing the ladybug at different distances from the center of the platform and measuring the time it takes to complete a full revolution, it becomes evident that the angular velocity varies based on the ladybug's distance.

A shorter time to complete a revolution indicates a higher angular velocity, while a longer time indicates a lower angular velocity. This demonstrates the relationship between the ladybug's distance from the center and its angular velocity.

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The UMTS (Universal Mobile Telecommunications System) and GSM (Global System for Mobile Communications) are two different cellular technologies used for mobile communication. The channel structure of the air interface in UMTS differs from GSM in several ways.

GSM:

In GSM, the air interface channel structure is based on a combination of time division multiple access (TDMA) and frequency division multiple access (FDMA). The spectrum is divided into multiple frequency channels, and each channel is further divided into time slots. Each time slot supports one user at a time, allowing multiple users to share the same frequency but with different time slots. This TDMA/FDMA combination is known as the TDMA frame structure.

UMTS:

UMTS, on the other hand, utilizes a different channel structure called wideband code division multiple access (WCDMA). WCDMA is a spread spectrum technique that employs a wider bandwidth compared to GSM. The entire available spectrum is shared among all users simultaneously, using different codes to differentiate between different users. This enables multiple users to access the same frequency at the time, resulting in a more efficient utilization of the spectrum.

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Answer: Foods that naturally are nutrient-rich include fruits and vegetables. Lean meats, fish, whole grains, dairy, legumes, nuts, and seeds also are high in nutrients.

Answer:

I don't know the answer but I needed the answer to that on a quiz and I downloaded sorcatic and it brings u to an app or website with the answer I hope this helps if you can't find the app than just tell me

Answer:

False.

Explanation:

An aurora is a natural electric phenomenon that creates bright and colorful light displays in the sky. These dramatic and colorful lights are created when electrically charged particles from solar winds enter the Earth's atmosphere and interact with gases in the atmosphere.

Answer:

The answer is "1.0748 and 1.0875".

Explanation:

Please find the complete question in the attachment file.

The incidence angle is [tex]i=45^{\circ}[/tex] for all colors When the angle is r, then use [tex]\frac{\sin{i}}{\sin{r}}=\frac{n_{o}}{n}[/tex] . Snell's rule Where [tex]n_{o}[/tex] is an outside material reflectance (same hue index) or n seems to be the crown glass index of the refraction, That index of inclination is [tex]90^{\circ}[/tex] as the light in color shifted behaver from complete inner diffraction to diffraction.

Whenever the external channel has a thermal conductivity for the red light, that's also

[tex]n_{o}=\frac{n_{r}\sin{45^{\circ}}}{\sin{90^{\circ}}}=\frac{1.520\times\sin{45^{\circ}}}{\sin{90^{\circ}}}=1.0748[/tex]

When outside the material has a refractive index, this happens with violet light.

[tex]n_{o}=\frac{n_{r}\sin{45^{\circ}}}{\sin{90^{\circ}}}=\frac{1.538\times\sin{45^{\circ}}}{\sin{90^{\circ}}}=1.0875[/tex]

In point a, The only red light flows out from the leaned face and the residual colors are mirrored mostly on prism for the primary benefits [tex]n_{o}=1.0748[/tex] (and slightly larger than that).

In point b, The only violet light is shown in the prism with the majority of the colors coming out from the sloping face for a scale similar to [tex]n_{o}= 1.0875[/tex] (and slightly smaller than this).

The specific strength and specific stiffness of the given fiber-reinforced composite are 2565 MPa/g and 17.62 GPa/g, respectively.

To determine the specific strength and specific stiffness, we need to calculate the strength and stiffness of the composite and then normalize them by the weight fraction of the fibers.

1. Calculate the strength of the composite:

The strength of the composite is determined by the strength of the fibers and the fiber volume fraction. Since the fibers are assumed to fail before the matrix, we can use the fiber strength to calculate the composite strength.

Composite strength = Fiber strength × Volume fraction fibers

Composite strength = 3500 MPa × 0.60

Composite strength = 2100 MPa

2. Calculate the stiffness of the composite:

The stiffness of the composite is determined by the properties of both the fibers and the matrix. We can calculate it using the rule of mixtures.

Composite modulus = (Volume fraction fibers × Fiber modulus) + ((1 - Volume fraction fibers) × Matrix modulus)

Composite modulus = (0.60 × 72.5 GPa) + (0.40 × 2.41 GPa)

Composite modulus = 43.5 GPa + 0.964 GPa

Composite modulus = 44.464 GPa

3. Calculate the specific strength and specific stiffness:

Specific strength = Composite strength / Composite density

Specific strength = (Composite strength / Fiber volume fraction) / (Fiber density + Matrix density)

Specific strength = (2100 MPa / 0.60) / (0.60 × 2.58 g/cm + 0.40 × 1.20 g/cm)

Specific strength = 3500 MPa/g

Specific stiffness = Composite modulus / Composite density

Specific stiffness = (Composite modulus / Fiber volume fraction) / (Fiber density + Matrix density)

Specific stiffness = (44.464 GPa / 0.60) / (0.60 × 2.58 g/cm + 0.40 × 1.20 g/cm)

Specific stiffness = 17.62 GPa/g

The specific strength and specific stiffness of the given fiber-reinforced composite are 2565 MPa/g and 17.62 GPa/g, respectively. These values indicate the strength and stiffness of the composite per unit weight of the material, taking into account the properties of both the fibers and the matrix.

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Answer:

The answer is B - the bending of rock layers happens due to stress, and this process is called folding. Faults are when it looks broken/displaced

The temperature rise, in degrees Celsius is determined as 1.7⁰.

The temperature rise, in degrees Celsius is calculated by applying principle of conservation of energy as follows;

Heat gained by the air = heat lost by the heater

mcΔθ = P x t

where;

The energy supplied to the heater is calculated as

E = P x t

E = 1700 w x 600 s

E = 1,020,000 J = 1,020 kJ

The temperature rise, in degrees Celsius is calculated as;

Δθ  = E / mc

Δθ  = ( 1020 ) / ( 320 x 1.87 )

Δθ  = 1.7⁰

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When the object is placed between 2F and F in front of a concave lens characteristic of the image formed by an object is virtual, therefore the correct option first option that the image is virtual.

It is the phenomenon of bending of light when it travels from one medium to another medium. The bending towards or away from the normal depends upon the medium of travel as well as the refractive index of the material.

Snell's law,

n₁sin(θ₁) = n₂sin(θ₂)

Where n is the refractive index and  θ represents angles

A concave lens is used to diverge the incident rays of light falling on it. because of this, the image formed by the concave lens is virtual.

These concave lenses are used in several days to day life applications such as cameras, telescopes, and eye glasses.

When the object is placed between 2F and F in front of a concave lens the characteristic of the image formed by an object is virtual. therefore the correct option first option is that the image is virtual.

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Answer:

the image is virtual

Explanation:

I got it right

Answer:

filament bulb, filament lamp

Explanation:

More length of a wire is a component that has a greater resistance as the current through it increases​.

The resistance of a long wire is greater than the resistance of a short wire because electrons collide with more ions present in the wire as they pass through. The moving electrons can collide with the ions present in the metal.

This makes more difficult for the current to flow and causes resistance in the wire so we can conclude that more length of a wire is a component that has greater resistance as more current passes through it.

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The rms current in the circuit is 0.0329 A, the phase angle between voltage and current in the circuit is approximately 2.53 degrees and the voltmeter reading across R is 201.15 V, and the voltmeter reading across C is 38.85 V.

What is a voltmeter?

A voltmeter is an electrical measuring instrument used to measure the voltage or potential difference between two points in an electric circuit. It is connected in parallel across the component or portion of the circuit where the voltage is to be measured.

Part A:

The rms current in the circuit (Irms) can be calculated using the formula:

Irms = Vrms / Z,

where Vrms is the rms applied voltage and Z is the impedance of the circuit.

The impedance of an RC circuit is given by:

Z = √(R² + (1 / (ωC))²),

where R is the resistance, C is the capacitance, and ω is the angular frequency.

Given:

Resistance, R = 6.10 kΩ = 6100 Ω,

Capacitance, C = 1.20 μF = 1.20 × 10^(-6) F,

RMS applied voltage, Vrms = 240 V,

Frequency, f = 60.0 Hz.

First, let's calculate the angular frequency:

ω = 2πf.

Substituting the given frequency value:

ω = 2π × 60.0 rad/s.

Now, we can calculate the impedance:

Z = √(R² + (1 / (ωC))²).

Substituting the given values:

Z = √((6100 Ω)² + (1 / (2π × 60.0 rad/s × 1.20 × 10^(-6) F))²).

Calculating:

Z ≈ 7277.61 Ω.

Finally, we can calculate the rms current:

Irms = Vrms / Z.

Substituting the given values:

Irms ≈ 240 V / 7277.61 Ω.

Calculating:

Irms ≈ 0.0329 A.

Therefore, the rms current in the circuit is approximately 0.0329 A.

Part B:

The phase angle (φ) between voltage and current in an RC circuit can be calculated using the formula:

tan(φ) = (1 / (ωRC)),

where R is the resistance, C is the capacitance, and ω is the angular frequency.

Substituting the given values:

tan(φ) = (1 / (2π × 60.0 rad/s × 6100 Ω × 1.20 × 10^(-6) F)).

Calculating:

tan(φ) ≈ 0.0444.

To find the phase angle φ, we take the inverse tangent (arctan) of the calculated value:

φ ≈ arctan(0.0444).

Calculating:

φ ≈ 2.53 degrees.

Therefore, the phase angle between voltage and current in the circuit is approximately 2.53 degrees.

Part C:

The voltmeter readings across R and C can be calculated using the voltage-divider rule.

The voltage across the resistor (VR) can be calculated as:

VR = Vrms * (R / Z).

Substituting the given values:

VR = 240 V * (6100 Ω / 7277.61 Ω).

Calculating:

VR ≈ 201.15 V.

The voltage across the capacitor (VC) can be calculated as:

VC = Vrms * (1 - (R / Z)).

Substituting the given values:

VC = 240 V * (1 - (6100 Ω / 7277.61 Ω)).

Calculating:

VC ≈ 38.85 V.

Therefore, the voltmeter reading across R is approximately 201.15 V, and the voltmeter reading across C is approximately 38.85 V.

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If Earth's mass decreased to one half its original mass, with no change in radius, then your weight would decrease to one half your original weight. Hence, option (A) is correct.

Centripetal acceleration is caused by constant change in direction.

An attribute of an object moving in a circular route is centripetal acceleration. Any object moving in a circle with an acceleration vector pointing in the direction of the circle's center is said to be experiencing centripetal acceleration.

You must have come across a lot of centripetal acceleration in your daily life. You experience centripetal acceleration as you drive in circles, and a satellite experiences centripetal acceleration when it orbits the planet. Being centered is referred to as being centripetal.

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The estimated temperature of the silica cylinder when operating is approximately 227,273 Kelvin.

To estimate the temperature of the silica cylinder in the radiant wall heater, we can use the Stefan-Boltzmann law, which relates the power radiated by a black body to its temperature. The formula is given by:

P = σ * A * T^4

Where:

P is the power radiated (in watts),

σ is the Stefan constant (6 x 10^-8 Wm^-2K^-4),

A is the surface area of the silica cylinder (in square meters),

T is the temperature of the cylinder (in Kelvin).

First, we need to calculate the surface area of the cylinder. The surface area of a cylinder is given by the formula:

A = 2πrh + πr^2

Where:

r is the radius of the cylinder (in meters),

h is the height of the cylinder (in meters).

Given that the radius (r) is 6 mm, which is 0.006 meters, and the length (h) is 0.6 meters, we can calculate the surface area:

A = 2 * π * 0.006 * 0.6 + π * (0.006)^2

A ≈ 0.227 square meters

Now, let's rearrange the Stefan-Boltzmann law to solve for the temperature (T):

T^4 = P / (σ * A)

T = (P / (σ * A))^(1/4)

Substituting the given power rating of 1.5 kW (1.5 * 10^3 W), and the calculated surface area (A ≈ 0.227), we get:

T ≈ (1.5 * 10^3) / (6 * 10^-8 * 0.227)^(1/4)

T ≈ (1.5 * 10^3) / (1.362 * 10^-8)^(1/4)

T ≈ (1.5 * 10^3) / 0.0066

T ≈ 227,273 Kelvin

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(a) The parity operator is Hermitian as it satisfies P† = P.

(b) Eigenfunctions of the parity operator with different eigenvalues are orthogonal.

(a) To prove that the parity operator is Hermitian, we must show that it satisfies the condition: P† = P, where P† denotes the Hermitian conjugate of the operator P.

The parity operator, denoted by P, is defined as follows:

Pψ(x) = ψ(-x),

where ψ(x) is the wavefunction.

To prove that P is Hermitian, we consider the Hermitian conjugate of the parity operator P†:

P†ψ(x) = [ψ(-x)]†.

Since we are dealing with complex conjugation, we can write this as:

P†ψ(x) = ψ*(-x),

where ψ*(x) represents the complex conjugate of the wavefunction ψ(x).

Comparing P†ψ(x) with Pψ(x), we can observe that they are equal except for the presence of the complex conjugate in P†ψ(x). However, the complex conjugate does not affect equality since it cancels out when taking the inner product or evaluating the integral.

Thus, P†ψ(x) = ψ*(-x) = ψ(x) = Pψ(x).

Since P†ψ(x) = Pψ(x), we can conclude that the parity operator P is Hermitian.

(b) To show that the eigenfunctions of the parity operator corresponding to different eigenvalues are orthogonal, we need to demonstrate that their inner product is zero.

Let ψ1(x) and ψ2(x) be two eigenfunctions of the parity operator with eigenvalues p1 and p2, respectively, where p1 ≠ p2.

The eigenvalue equation for the parity operator can be written as:

Pψ(x) = pψ(x).

Considering the inner product of ψ1(x) and ψ2(x) and using the definition of the parity operator, we have:

⟨ψ1|ψ2⟩ = ∫ ψ1*(x)ψ2(x) dx.

Now, we can substitute the definition of the parity operator into this inner product:

⟨ψ1|ψ2⟩ = ∫ ψ1*(-x)ψ2(x) dx.

Since p1 ≠ p2, the eigenvalues of ψ1(x) and ψ2(x) are different. This implies that their corresponding eigenfunctions are distinct and do not have the same symmetry properties under parity.

When integrating the product ψ1*(-x)ψ2(x) over the entire domain, the integrand will exhibit oscillatory behavior due to the mismatch in the symmetry of the two functions.

As a result, the integral ∫ ψ1*(-x)ψ2(x) dx will evaluate to zero, indicating that the eigenfunctions of the parity operator corresponding to different eigenvalues are orthogonal.

Therefore, we can conclude that the eigenfunctions of the parity operator with different eigenvalues are orthogonal.

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The period of the pendulum, considering the small angle approximation, is approximately 2.45 seconds (s). This is calculated using the formula T = 2π√(L/g), where L is the effective length of the pendulum and g is the acceleration due to gravity.

To calculate the period, we can use the formula for the period of a simple pendulum, which is given by T = 2π√(L/g), where T is the period, L is the length of the pendulum, and g is the acceleration due to gravity.

In this case, the length of the pendulum is 2.3 m. However, we need to consider the effective length of the pendulum due to the position of mass M2. The distance of M2 from the pivot point is (3/5)L = (3/5)(2.3) = 1.38 m.

Therefore, the effective length of the pendulum is L - (1.38) = 0.92 m.

Substituting the values into the formula, we have T = 2π√(0.92/9.8) ≈ 2.45 s.

Thus, the period of this pendulum in the small angle approximation is approximately 2.45 seconds.

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renewable sources represent approximately 11% of global energy consumption. However, please note that the percentage may have changed since then, as the adoption and development of renewable energy sources continue to evolve.

The percentage of global energy consumption from renewable sources is subject to change as advancements in renewable technologies, policy changes, and shifts in energy markets occur. It is always important to consult the latest data and reliable sources for the most up-to-date information on global energy consumption and the proportion contributed by renewable sources. as the adoption and development of renewable energy sources continue to evolve. It's always recommended to refer to the most recent and reliable sources for the most up-to-date information on global energy consumption.

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The minimum horsepower required to drag the 370-kg box at a speed of 1.20 m/s is the calculated value from the equation above.

To determine the minimum horsepower required, we need to calculate the force needed to overcome friction and move the box at the given speed.

The force required to overcome friction can be calculated using the equation:

F_friction = coefficient of friction * normal force

The normal force can be calculated as the weight of the box:

normal force = mass * gravitational acceleration

Substituting the given values:

normal force = 370 kg * 9.8 m/s^2

Next, we can calculate the force required to maintain a constant speed:

F = mass * acceleration

Since the box is moving at a constant speed, the acceleration is zero. Therefore, the force required to maintain the speed is zero.

The minimum force required is the force to overcome friction, so:

F_required = F_friction

Substituting the values:

F_required = 0.45 * (370 kg * 9.8 m/s^2)

Now, we need to convert this force to horsepower. One horsepower is equal to 745.7 watts. Therefore, we can calculate the minimum horsepower required:

Horsepower = F_required * (1 watt / 745.7) * (1 horsepower / 1 watt)

Finally, substituting the values and calculating:

Horsepower = (0.45 * (370 kg * 9.8 m/s^2)) / 745.7

Hence, the minimum horsepower required to drag the 370-kg box at a speed of 1.20 m/s is the calculated value from the equation above.

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Answer & Explanation:

In science, rationality and creativity work together. Creativity allows us to view and solve problems with innovation and openness. Scientific theories often came from sparks of creative thinking and bold yet logical processes.

a) Calculation of temperature at the fat-inner fur boundaryThe rate of heat flow is given by:

[tex]q =\frac{kA\Delta T}{d}[/tex]

where, k = thermal conductivity; A = surface area; ΔT = temperature difference and d = thicknessSince the rate of heat flow is given to be 51.4 W, we can obtain the temperature difference from the given data.

[tex]ΔT = \frac{30.9 - 2.8}{\ln \frac{3.9}{1.6/2}} ≈ 3.6°C[/tex]

Now, substituting the given values of A, d and k, we get

[tex]51.4 = \frac{0.200 \pi (1.6)^{2} \times 3.6}{0.039} × (T1 - 30.9)[/tex]

where T1 is the required temperature at the fat-inner fur boundarySimplifying, we getT1 ≈ -9.7°Cb) Calculation of thickness of air layerAssuming the layer of air to be stationary and isothermal, the rate of heat flow can be calculated using the following equation:q = hAΔTwhere, h = heat transfer coefficientThe heat transfer coefficient, h can be calculated using the relation:

[tex]q = [\frac{kA\Delta T}{d} = hAΔT ⇒ h =\frac{k}{d}\\[/tex]

Using this, we can obtain the heat transfer coefficient, which is approximately 0.7 W/(m².K)Using the relation above, we can write:

[tex]51.4 = 0.7 × (4π(1.6/2)²) × ΔT × d[/tex]

where ΔT is the temperature difference and d is the thickness of the air layerSolving for d, we getd ≈ 1.2 cmTherefore, the thickness of the air layer should be around 1.2 cm so that the bear loses heat at a rate of 51.4 W.

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After seven half-lives, a significant percentage (approximately 99.22%) of a radioactive species would be found as daughter material, while only a small fraction (approximately 0.78%) of the parent material would remain.

The missing item to complete the beta decay reaction would be the radioactive parent nucleus. Without knowing the specific parent nucleus involved, it is challenging to provide the complete reaction equation. In beta decay, a radioactive parent nucleus undergoes the transformation where a beta particle (electron) is emitted, resulting in the formation of a daughter nucleus.

Now let's discuss the percentage of a radioactive species that would be found as daughter material after seven half-lives. The half-life of a radioactive substance is the time it takes for half of the initial amount of the substance to decay. Each half-life represents a 50% reduction in the amount of the parent material remaining.

After one half-life, 50% of the parent material will have decayed, leaving 50% as the daughter material. After two half-lives, another 50% of the remaining parent material will decay, resulting in 25% of the original parent material and 75% as the daughter material. This pattern continues for each subsequent half-life.

Therefore, after seven half-lives, the remaining parent material will be reduced to (1/2)^7 = 1/128 ≈ 0.78% of the original amount. Consequently, approximately 99.22% of the radioactive species would have decayed into the daughter material after seven half-lives.

It is important to note that the specific percentage of daughter material after seven half-lives will depend on the particular radioactive species and its decay characteristics. Different radioactive substances have different half-lives, so the percentage of daughter material after seven half-lives will vary between different radioactive species.

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The displacement current (Id) between the square plates of the capacitor is approximately 7.136×10⁻¹¹ Amperes.

The displacement current (Id) between the square plates of a capacitor with sides measuring 7.6 cm, when the electric field is changing at a rate of 1.4×10⁶ V/m⋅s, can be calculated using Maxwell's equations.

The displacement current (Id) is a term introduced by James Clerk Maxwell to account for the changing electric field in a region where a current is not flowing. According to Maxwell's equations, the displacement current is given by the formula:

Id = ε₀ * dΦE/dt

where ε₀ is the permittivity of free space (approximately 8.854×10⁻¹² F/m) and dΦE/dt represents the rate of change of the electric flux through the capacitor plates.

To calculate dΦE/dt, we need to consider the area of the plates and the rate of change of the electric field. Given that the plates are square and have sides measuring 7.6 cm, the area of each plate is (7.6 cm)² = 57.76 cm² = 5.776×10⁻³ m².

The electric field change rate is given as 1.4×10⁶ V/m⋅s. To find dΦE/dt, we multiply this value by the area of the plates:

dΦE/dt = (1.4×10⁶ V/m⋅s) * (5.776×10⁻³ m²) = 8.0864 A

Finally, we can calculate the displacement current using the formula:

Id = ε₀ * dΦE/dt = (8.854×10⁻¹² F/m) * (8.0864 A) = 7.136×10⁻¹¹ A

Therefore, the displacement current (Id) between the square plates of the capacitor is approximately 7.136×10⁻¹¹ Amperes.

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The maximum efficiency of the heat engine with operating temperatures of 580°C and 380°C. is 4.5%.

The maximum efficiency of a heat engine with operating temperatures of 580°C and 380°C can be calculated using the Carnot efficiency formula.

The Carnot efficiency formula is given by:

Efficiency = 1 - (Tc / Th)

where Tc is the temperature of the cold reservoir and Th is the temperature of the hot reservoir.

Plugging in the given temperatures:

Efficiency = 1 - (380°C / 580°C) = 1 - 0.655 ≈ 0.345 ≈ 34.5%

Therefore, the correct answer is 34.5%, which represents the maximum efficiency of the heat engine with operating temperatures of 580°C and 380°C.

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Answer:

Explanation:

Add pqq to both sides

3t = pqq + 2 pn                       Pull out p as a common factor.

3t = p(qq + 2n)                       Divide by qq + 2n

3t/(qq + 2n)

Answer:

5,000-Hz

Explanation: