The wing area divided by the span of a wing is called:A) fineness ratio.B) mean cord.C) aspect ratio.D) wash out.

Answer:

Horizontal force = 89.2 N

Explanation:

The frictional force = coefficient of friction * magnitude of the force (weight of the body) * cos theta

Substituting the given values, we get -

Frictional Force = 0.3*300 * cos 25 = 89.2 N

Horizontal force = 89.2 N

Answer:

To counter the behavior of a high Mach individual in my workplace, I could put the individual in charge of a project by himself, and don't let others work with him.

Explanation:

A high Mach individual is one who exhibits a manipulative and self-centered behavior.   The personality trait is characterized by the use of manipulation and persuasion to achieve power and results.  But, such individuals are hard to be persuaded.  They do not function well in team settings and asking them to agree to terms is very difficult.  "The presence of Machiavellianism in an organisation has been positively correlated with counterproductive workplace behaviour and workplace deviance," according to wikipedia.com.

Mach is an abbreviation for Machiavellianism.  Machiavellianism is referred to in psychology as a personality trait which sees a person so focused on their own interests that they will manipulate, deceive, and exploit others to achieve their selfish goals.  It is one of the Dark Triad traits.  The others are narcissism and psychopathy, which are very dangerous behaviors.

The resulting non-ambiguous grammar is S → 1S | AA, A → 1A | BB, and B → 0B | ε.

To construct a non-ambiguous grammar generating the language {w ϵ {0,1}* | every prefix of w contains no more 0s than 1s}, we need to follow these steps:

The non-ambiguous grammar generating the language {w ϵ {0,1}* | every prefix of w contains no more 0s than 1s} is as follows:

S → 1S | AAS → 0A | εA → 1A | BBA → εB → 0B | ε

S → 1S | AA: This rule states that every string in the language should start with 1s or a string in A followed by an

A.A → 1A | BB: This rule generates strings that have no more 0s than 1s. The strings generated by this rule contain any number of 1s, and any prefix has no more 0s than

1s.B → 0B | ε: This rule generates strings that contain no more 0s than 1s.

The strings generated by this rule can contain any number of 1s, but they must have the same number of 0s or more 0s than 1s.

So, the non-ambiguous grammar generating the language {w ϵ {0,1}* | every prefix of w contains no more 0s than 1s} is S → 1S | AA, A → 1A | BB, and B → 0B | ε.

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The number of commutator bars for a 4-pole, 2-layer, DC lap winding with 20 slots and one conductor per layer exists 20

Lap Winding is one kind of winding with two layers, and it is used in electric machines. Every coil in the engine is allied in series with the one nearby coil to it. The applications of lap winding mainly contain low voltage as well as high current devices.

Advantages of Lap Winding

The advantages of lap windings contain: This winding is necessarily needed for large current applications because it has more parallel paths. It is suited for low voltage and high current generators.

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Answer:

The purpose of Customs Duty is to protect each country's economy, residents, jobs, environment, etc., by controlling the flow of goods, especially restrictive and prohibited goods, into and out of the country.

According to the question of theorem in which we have to convert, then the PDA is given below:

A theorem is a statement in mathematics that has been proven to be true using accepted methods of proof. It can be used to make predictions about various mathematical concepts and to prove the validity of other mathematical theorems. A theorem is the result of a logical argument and is often comprised of previously established facts or laws.  A theorem is a fundamental building block in mathematics, as it is used to prove other theorems.

PDA: Q={q0,q1,q2,q3,q4,q5}

Σ={a,b}

Γ={a,b,X,R,S,T,ε}

q0=q0

q5=accept state

δ:(q0,a,ε)->(q1,X,RST)

   (q1,a,R)->(q1,X,RS)

   (q1,b,R)->(q1,X,ST)

   (q1,a,S)->(q2,ε,aTb)

   (q1,b,S)->(q3,ε,bTa)

   (q2,a,T)->(q2,ε,a)

   (q2,b,T)->(q2,ε,ε)

   (q3,a,T)->(q3,ε,ε)

   (q3,b,T)->(q3,ε,b)

   (q2,a,X)->(q4,ε,ε)

   (q2,b,X)->(q4,ε,ε)

   (q3,a,X)->(q4,ε,ε)

   (q3,b,X)->(q4,ε,ε)

   (q4,a,ε)->(q1,X,RS)

   (q4,b,ε)->(q1,X,ST)

   (q1,ε,X)->(q5,ε,ε)

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Try answering with a Twisted-pair cable.

Answer: i believe it’s acoustics

Explanation:

Answer:

This is an asynchrnous 3-bit counter. Just note that this design is different and works differently than its synchronous counterpart. It's an easier design than its synchronous counterpart, and is not as reliable because it has delays.

Answer:

Completed load manifest, dispatch release and flight plan

Answer:

9A

Explanation:

The minimum required width of the basin should be approximately 40,285.71 square meters to ensure the settling of 10 μm diameter particles within the tank's depth.

To determine the minimum required width of the rectangular sedimentation tank, we need to consider the settling velocity of the 10 μm diameter particles and ensure that they settle within the tank's depth. The settling velocity can be calculated using Stokes' law:

v = (2/9) * (g * (ρp - ρw) * d^2) / η,

where v is the settling velocity, g is the acceleration due to gravity (9.81 m/s^2), ρp is the particle density (1.2 g/mL), ρw is the water density (1 g/mL), d is the particle diameter (10 μm = 10 × 10^-6 m), and η is the dynamic viscosity of water at 20°C (taken as 1.002 × 10^-3 Pa·s).

First, let's convert the particle density to kg/m^3:

ρp = 1.2 g/mL * (10^3 kg/g) * (10^-6 m^3/mL) = 1200 kg/m^3.

Substituting the values into Stokes' law, we can calculate the settling velocity:

v = (2/9) * (9.81 m/s^2 * (1200 kg/m^3 - 1000 kg/m^3) * (10 × 10^-6 m)^2) / (1.002 × 10^-3 Pa·s) = 4.96 × 10^-7 m/s.

Next, we need to ensure that the particles settle within the sedimentation tank's depth. Given a tank depth of 3.5 m, the time required for settling can be calculated as:

t = depth / v = 3.5 m / (4.96 × 10^-7 m/s) = 7.05 × 10^6 s.

Now, let's determine the volume of water that flows through the plant in the settling time:

volume = flow rate * time = 0.100 m^3/s * (7.05 × 10^6 s) = 705,000 m^3.

To maintain proper settling within the tank, the width (W) of the tank should be such that the settling volume is accommodated:

settling volume = length * width * depth.

Rearranging the formula to solve for the width:

width = settling volume / (length * depth) = 705,000 m^3 / (5 * 3.5 m) = 40,285.71 m^2.

Therefore, the minimum required width of the basin should be approximately 40,285.71 square meters to ensure the settling of 10 μm diameter particles within the tank's depth.

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An ordered set of pairs or a continuous line can both be used to represent a function on a graph.

An example of a function is the line y = 2x, which multiplies an input value by two to get an output value. Use the vertical line test to decide if a graph accurately depicts a function. The graph is a function if a vertical line drawn across it is moved and only ever touches it at one point. The graph is not a function if the vertical line crosses it at more than one location. if a vertical line drawn anywhere on a relation's graph only encounters one point of intersection.

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Answer:

In physics, equations of motion are equations that describe the behavior of a physical system in terms of its motion as a function of time. More specifically, the equations of motion describe the behavior of a physical system as a set of mathematical functions in terms of dynamic variables

Explanation:

1. The general attitude dynamic equation is given by:
τ = I * α + ω x (I * ω)

2. Three attitude control methods are:
a) Reaction wheels
b) Thrusters
c) Control moment gyroscopes

Explanation:
The general attitude dynamic equation represents the relationship between external torques (τ), inertia tensor (I), angular acceleration (α), and angular velocity (ω) of a rigid body in space. It is crucial for understanding and controlling the orientation of spacecraft or satellites.

a) Reaction wheels: These are spinning rotors used to change the orientation of a spacecraft by applying a torque in the opposite direction.
Advantages: They provide precise control, are energy-efficient, and produce no exhaust.
Disadvantages: Limited torque capacity, saturation, and require periodic desaturation using thrusters.

b) Thrusters: Small rocket engines that produce thrust by expelling propellant. They can be used for attitude control by generating torques around the spacecraft's center of mass.
Advantages: Provide high torque capability and rapid response.
Disadvantages: Limited propellant supply, less precise control, and produce exhaust that can contaminate sensitive instruments.

c) Control moment gyroscopes (CMGs): Rotating flywheels mounted on gimbals that generate torques by changing the angular momentum of the flywheels.
Advantages: High torque capacity, precise control, and no propellant required.
Disadvantages: Complex mechanical design, sensitive to gimbal lock, and require more power than reaction wheels.

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Answer:

maximum torque of metal

Explanation:

Thus, if it snows, I use the metro. Finally, p->r————if it snows and I am late to work because q->r————when I take the train then I am behind schedule. Well, at last! There is not snow, so p.

Activity that a man habitually engages in to make a living: activity whereby a person uses strength or intellect to do or do anything. persons seeking employment.

In conclusion, we may conclude that the term "job" refers to a specific employment function or function, such as that of a cook, teacher, or banker, but the term "work" refers more broadly to the activities you engage in. Contrary to popular belief, not all occupations need you to perform work.

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Answer:

C) a winding connected in series with the armature.

Explanation:

In a series motor, an electromagnet is used as a stator to generate its magnetic field. The field coil of this stator are connected through a commutator in series with the rotor windings. This stator which is the armature windings will conduct AC even on a DC machine, due to the  periodically reverses current direction (commutation) or due to electronic commutation (as in brushless DC motors).

Answer:

Cool I think u should do Marvel first

Answer:

Option B

Explanation:

Atoms of ferromagnetic materials have north and south pole but these atoms are oriented in random directions due to which they do no exhibit magnetic properties until unless they are brought into influence of any external temporary or permanent magnetic field.

Under the influence of external magnetic force, the atoms of the ferromagnetic material get oriented in a particular direction.

Hence, option B is correct

If a W18x119 steel section is used as a compression member with one end fixed and the other end pinned, and the length of the member is 12 feet, the available compressive strength can be determined for A992 steel.

To calculate the available compressive strength, we need to consider the buckling behavior of the member. In this case, the buckling mode is Euler buckling, which occurs when the critical stress of the member is reached.

The critical stress for Euler buckling can be calculated using the formula:

σc = (π^2 * E) / (K * L / r)^2

Where:

σc is the critical stress

E is the modulus of elasticity of the material (for A992 steel, it is approximately 29,000 ksi)

K is the effective length factor (for a pin-ended compression member, K is 1.0)

L is the length of the member (12 feet in this case, which is 144 inches)

r is the radius of gyration of the W18x119 section, which can be obtained from steel section tables or calculated using geometric properties of the section.

Once the critical stress is determined, the available compressive strength is typically taken as a fraction of the critical stress, depending on the design safety factor specified by the applicable design code. The design safety factor varies depending on the specific design requirements and standards being used.

By plugging in the values and performing the calculations, the available compressive strength for the given W18x119 section made of A992 steel can be determined.

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This question is incomplete, the missing diagram is uploaded along this answer below.

Answer:

the forces required to keep the artery in place is 1.65 N

Explanation:

Given the data in the question;

Inlet velocity V₁ = 50 cm/s = 0.5 m/s

diameter d₁ = 15 mm = 0.015 m

radius r₁ = 0.0075 m

diameter d₂ = 11 mm = 0.011 m

radius r₂ = 0.0055 m

A₁ = πr² = 3.14( 0.0075 )² =  1.76625 × 10⁻⁴ m²

A₂ = πr² = 3.14( 0.0055 )² =  9.4985 × 10⁻⁵ m²

pressure at inlet P₁ = 110 mm of Hg = 14665.5 pascal

pressure at outlet P₂ = 95 mm of Hg = 12665.6 pascal

Inlet volumetric flowrate = A₁V₁ = 1.76625 × 10⁻⁴ × 0.5 = 8.83125 × 10⁻⁵ m³/s

given that; blood density is 1050 kg/m³

mass going in m' = 8.83125 × 10⁻⁵ m³/s × 1050 kg/m³ = 0.092728 kg/s

Now, using continuity equation

A₁V₁ = A₂V₂

V₂ = A₁V₁ / A₂ = (d₁/d₂)² × V₁

we substitute

V₂ =  (0.015 / 0.011 )² × 0.5

V₂ = 0.92975 m/s

from the diagram, force balance in x-direction;

0 - P₂A₂ × cos(60°) + Rₓ = m'( V₂cos(60°) - 0 )    

so we substitute in our values

0 - (12665.6 × 9.4985 × 10⁻⁵)  × cos(60°) + Rₓ = 0.092728( 0.92975 cos(60°) - 0 )    

0 - 0.6014925 + Rₓ =  0.043106929 - 0

Rₓ = 0.043106929 + 0.6014925

Rₓ = 0.6446 N

Also, we do the same force balance in y-direction;

P₁A₁ - P₂A₂ × sin(60°) + R\(_y\) = m'( V₂sin(60°) - 0.5 )  

we substitute

⇒ (14665.5 × 1.76625 × 10⁻⁴) - (12665.6 × 9.4985 × 10⁻⁵) × sin(60°) + R\(_y\) = 0.092728( 0.92975sin(60°) - 0.5 )

⇒ 1.5484 + R\(_y\) = 0.092728( 0.305187 )

⇒ 1.5484 + R\(_y\) = 0.028299    

R\(_y\) = 0.028299 - 1.5484

R\(_y\) = -1.52 N

Hence reaction force required will be;

R = √( Rₓ² + R\(_y\)² )

we substitute

R = √( (0.6446)² + (-1.52)² )

R = √( 0.41550916 + 2.3104 )

R = √( 2.72590916 )

R = 1.65 N

Therefore, the forces required to keep the artery in place is 1.65 N

Answer:

Fourier coefficient, Ck:

\({ \rm{ c_{k}} = \int ^{ \infin} _{ - \infin } \{x(t) {e}^{jk \omega _{0} t} \} }\)

Fourier transform:

\({ \rm{x( \omega) = \int ^{ \infin} _{ - \infin} } \{x(t) {e}^{j \omega} t} \}\)

The probability that a randomly selected male student is from the College at UVA is approximately 58.73%.

To find the probability, we need to consider the proportion of male students in each school and then calculate the proportion of male students specifically in the College. Given the percentages provided, we know that 73% of all undergraduates are in the College.

Therefore, if we assume an equal number of male and female students within each school, we can conclude that approximately 73% of male students at UVA are in the College.

However, we also need to consider the gender distribution within each school. We are told that 59% of students in the College are female. By subtracting this percentage from 100%, we can determine that approximately 41% of students in the College are male.

Next, we calculate the proportion of male students in the entire university by multiplying the percentage of male students in the College (41%) by the overall percentage of students in the College (73%). This gives us an estimate of 29.93% (0.41 * 0.73) of male students at UVA who are in the College.

Finally, to find the probability of a randomly selected male student being from the College, we divide the number of male students in the College by the total number of male students at UVA. Since we are only considering male students, we can exclude the gender distribution in other schools. The resulting probability is approximately 58.73% (29.93% divided by 51%).

In summary, the probability that a randomly selected male student is from the College at UVA is approximately 58.73%.

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Answer:

Q = [ mCp ( ΔT) ] \(_{cooling water }\)

(ΔT)\(_{cooling water}\) and  Q  is given

\(m_{cooling water}\)  = \(\frac{Q}{Cp[ T_{out} - T_{in} ] }\)

next the rate of condensation of the steam

Q = [ m\(h_{fg}\) ]\(_{steam}\)

  \(m_{steam} = \frac{Q}{h_{fg} }\)

Total resistance of the condenser is

R = \(\frac{Q}{change in T_{cooling water } }\)

Explanation:

How will the rate of condensation of the steam and the mass flow rate of the cooling water can be determined

Q = [ mCp ( ΔT) ] \(_{cooling water }\)

(ΔT)\(_{cooling water}\) and  Q  is given

\(m_{cooling water}\)  = \(\frac{Q}{Cp[ T_{out} - T_{in} ] }\)

next the rate of condensation of the steam

Q = [ m\(h_{fg}\) ]\(_{steam}\)

  \(m_{steam} = \frac{Q}{h_{fg} }\)

Total resistance of the condenser is

R = \(\frac{Q}{change in T_{cooling water } }\)

Answer:

Assume a value of 0.22 for the strain-hardening exponent, n.

Explanation:

Answer:

Operating Pressure P = 793.716 mmHg

Y_Benzene y1 = 0.541

Explanation:

Given that;

liquid phase leaving the evaporator = 32.5 mole%

Equi Temp T = 99.0°C = 99 + 273.15 = 372.15 K

Now let 1 and 2 represent Benzene and Toluene respectively.

Antoine's Constant for these components are;

COMPONENETS        A                B                    C

Benzene 1             4.72583     1660.652        -1.461

Toluene  2            4.07827     1343.943         -53.773

Antoine's equation is expressed as;

Ps = 10^(A - (B/(T+C)))

Ps is in Bar and T is in Kelvin

so

P1s = 10^( 4.72583 - (1660.652/(372.15 - (-1.461)))) = 1.7617 Bar

P2s = 10^( 4.07827 - (1343.943/(372.15 - (-53.773)))) = 0.7195 Bar

now here, liquid leaving and vapor are both in equilibrium

composition of liquid leaving are;

X1 = 32.5%    = 0.325

X2 = 1 - X1 = 1 - 0.325 = 0.675

Now

Raoult's Law is expressed as;

p × y1=x1 × pis     for all components

So for Benzene ; p × y1=x1 × p1s   ------let this be equation 1

for Toluene ; p × y2=x2 × p2s   ------let this be equation 2

lets add equ 1 and 2

p × y1=x1 × p1s + p × y2=x2 × p2s

p(y1 + y2) = x1 × p1s + x2 × p2s

buy y1 + y2 = 1

therefore we substitute

p(1) = 0.325 × 1.7617 + 0.675 × 0.7195 = 1.0582 Bar

we know that 1 Bar = 750.062 mmHg

so p = 1.0582 × 750.062

p = 793.716 mmHg

Also from equation 1

p × y1=x1 × p1s

y1 = (x1 × p1s) / p

y1 = (0.325 × 1.7617) / 1.0582

y1 = 0.541

Therefore;

Operating Pressure P = 793.716 mmHg

Y_Benzene y1 = 0.541

Answer:

volunteer coordinator

Explanation:

because they are volunteering for that and in most of the cases they do not expect to be paid

The thickness of the foil is 0.00516 mm.

To calculate the thickness of the foil using the formula of volume of a cuboid.

Where:

Make n the subject of the equation

From the question,

Given:

Substitute these values into equation 2

Hence, The thickness of the foil is 0.00516 mm.
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