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GarryVolchara [31]
3 years ago
12

Consider a NACA 2412 airfoil in a low-speed flow at zero degrees angle of attack and a Reynolds number of 8.9·106 . Calculate th

e percentage of drag from pressure drag due to flow separation (form drag). Assume a fully turbulent boundary layer over the airfoil. Assume that the airfoil is thin enough so that the skin-friction drag can be estimated by the flat-plate results discussed earlier. Now consider the same airfoil at an angle of attack of 6 degrees. Again, calculate the percentage of drag from pressure drag due to flow separation. What does this tell you about the rapid increase in drag coefficient as the angle of attack increases?
Engineering
1 answer:
Fofino [41]3 years ago
3 0

Answer:

a) pressure drag is zero (0)

b) pressure drag is 20%

Explanation:

Ans) Given,

NACA 2412 airfoil

Re = 8.9 x 10^6

We know, for turbulent flow ,drag coefficient, Cdf = 0.074 / Re^0.2

=> Cdf = 0.074 / (8.9 x 10^6)^0.2

=> Cdf = 0.003

For both side of plate, Cd = 2 x 0.003 = 0.006

For zero degree angle of attack for NACA 2412, Cdf = 0.006

Also, Cd = Cdf + Cdp

=> 0.006 = 0.006 + Cdp

=> Cdp = 0

Hence, pressure drag is zero

Now, for zero degree angle of attack for NACA 2412, Cd = 0.0075

Also, Cd = Cdf + Cdp

=> 0.0075 = 0.006 + Cdp

=> Cdp = 0.0075 - 0.006

=> Cdp = 0.0015

Hence, Pressure drag percentage = (Cdp / Cdf) x 100

=> Pressure drag percent = (0.0015/0.0075) x 100 = 20 %

Hence, pressure drag is 20% of pressure drag due to flow seperation  Ans) Given,

NACA 2412 airfoil

Re = 8.9 x 10^6

We know, for turbulent flow ,drag coefficient, Cdf = 0.074 / Re^0.2

=> Cdf = 0.074 / (8.9 x 10^6)^0.2

=> Cdf = 0.003

For both side of plate, Cd = 2 x 0.003 = 0.006

For zero degree angle of attack for NACA 2412, Cdf = 0.006

Also, Cd = Cdf + Cdp

=> 0.006 = 0.006 + Cdp

=> Cdp = 0

Hence, pressure drag is zero

Now, for zero degree angle of attack for NACA 2412, Cd = 0.0075

Also, Cd = Cdf + Cdp

=> 0.0075 = 0.006 + Cdp

=> Cdp = 0.0075 - 0.006

=> Cdp = 0.0015

Hence, Pressure drag percentage = (Cdp / Cdf) x 100

=> Pressure drag percent = (0.0015/0.0075) x 100 = 20 %

Hence, pressure drag is 20% of pressure drag due to flow seperation  

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Explanation:i helped

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3 years ago
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a solid circular shaft 150 mm diameter transmits a torque of 29820.586 N.m. find the maximum shear stress
bezimeni [28]

Answer:

45 Mpa

Explanation:

The maximum shear stress, \tau_{max}is given by

\tau_{max}=\frac {16T}{\pi d^{3}}

Where T is the torque and d is the diameter.

Substituting  29820.586 N.m for T and 0.15m for d then we obtain

\tau_{max}=\frac {16\times 29820.586}{\pi \times 0.15^{3}}=44999999.22\approx 45 Mpa

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4 years ago
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VashaNatasha [74]

Answer: C

Explanation:

5 0
3 years ago
A commercial refrigerator with refrigerant-134a as the working fluid is used to keep the refrigerated space at -30C by rejecting
chubhunter [2.5K]

Answer:

a) x = 0.4795

b) QL = 5.85 KW

c) COP = 2.33

d) QL_max = 12.72 KW

Explanation:

Solution:-

- Assuming the steady state flow conditions for both fluids R-134a and water.

- The thermodynamic properties remain constant for respective independent intensive properties.

- We will first evaluate the state properties of the R-134a and water.

- Compressor Inlet, ( Saturated Vapor ) - Ideal R-134a vapor cycle

              P1 = 60 KPa, Tsat = -36.5°C  

              T1 = -34°C , h1 = hg = 230.03 KJ/kg

              Qin = 450 W - surrounding heat  

- Condenser Inlet, ( Super-heated R-134a vapor ):

              P2 = 1.2 MPa , Tsat = 46.32°C  

              T2 = 65°C   , h2 = 295.16 KJ/kg

- Condenser Outlet, ( Saturation R-134a point ):

             P3 = P2 = 1.2 MPa , Tsat = 46.32°C

             T3 = 42°C   , h3 = hf = 111.23 KJ/kg

- R-134a is throttled to the pressure of P4 = compressor pressure = P1 = 60 KPa by an "isenthalpic - constant enthalpy pressure reduction" expansion valve.

- Inlet of Evaporator - ( liquid-vapor state )

             P4 = P1 = 60 KPa, hf = 3.9 KJ/kg , hfg = 223.9 KJ/kg

             h4 = h3 = 111.23 KJ/kg

- The quality ( x ) of the liquid-vapor R-134a at evaporator inlet can be determined:

             x4 = ( h4 - hf ) / hfg

             x4 = ( 111.23 - 3.9 ) / 223.9

             x4 = 0.4795      Answer ( a )        

- Water stream at a flow rate flow ( mw ) = 0.25 kg/s is used to take away heat from the R-134a.

- Condenser Inlet, ( Saturated liquid water ):

             Ti = 18°C , h = hf = 75.47 KJ/kg  

- Condenser Outlet, ( Saturated liquid water ):

             To = 26°C , h = hf = 108.94 KJ/kg

- Since the heat of R-134a was exchanged with water in the condenser. The amount of heat added to water (Qh) is equal to amount of heat lost from refrigerant R-134a.

- Apply thermodynamic balance on the R-134a refrigerant in the condenser:

             Qh = flow (mr) * [ h2 - h3 ]

Where,

flow ( mr ) : The flow rate of R-134a gas in the refrigeration cycle

             flow ( mr ) = Qh / [ h2 - h3 ]

             flow ( mr ) = 8.3675 / [ 295.16 - 111.23 ]

             flow ( mr ) = 0.0455 kg/s

- The cooling load of the refrigeration cycle ( QL ) is determined from energy balance of the cycle net work input ( Compressor work input ) - "Win" and the amount of heat lost from R-134a in condenser ( Qh ).

- Apply the thermodynamic balance for the compressor:

           

            Win = flow ( mr )*[ h2 - h1 ] - Qin

            Win = 0.0455*[ 295.16 - 230.03] KW - 0.45 KW

            Win = 2.513 KW

- The cooling load ( QL ) for the refrigeration cycle can now be calculated. Apply thermodynamic balance for the refrigeration cycle:

            QL = Qh - Win

            QL = 8.3675 - 2.513

            QL= 5.85 KW  .... Refrigeration Load, Answer ( b )

- The COP of the refrigeration cycle is calculated as the ratio of useful work and total work input required:

           

             COP = QL / Win

             COP = 5.85 / 2.513

             COP =  2.33      Answer ( c )            

- For a compressor to be working at 100% efficiency or ideal then the maximum COP for the refrigeration cycle would be:

           

             COP_max = [ TL ] / [ Th - TL ]

Where,

            TL : The absolute temperature of heat sink, refrigerated space

            TH : The absolute temperature of heat source, water inlet

                 

            COP_max = [ -30+273 ] / [ (18+273) - (-30+273) ]          

            COP_max = 5.063

- The theoretical ideal refrigeration load ( QL max ) would be:

     

           COP_max = QL_max / Win

           QL_max = Win*COP_max

           QL_max = 2.513*5.063

           QL_max = 12.72 KW     Answer ( d )

5 0
4 years ago
If the atomic radius of copper is 0.128 nm, calculate the volume of its unit cell in cubic meters.
Alex_Xolod [135]

Answer:

Volume of face centered cubic cell=4.74531*10^{-29} m^3

Explanation:

Consider the face centered cubic cell:

1 atom at each corner of cube.

1 atom at center of each face.

Consider the one face (ABCD) as shown in attachment for calculation:

Length of the all sides of face centered cubic cell is L.

Volume of face centered cubic cell= L^3

Now Consider the figure shown in attachment:

According to Pythagoras theorem on ΔADC.

L^{2}+L^2=(4a)^2     (a is the atomic radius)

L=\frac{4a}{\sqrt{2}} (Put in the formula of Volume)

Volume of face centered cubic cell= L^3

Volume of face centered cubic cell= (\frac{4a}{\sqrt{2}})^3

Volume of face centered cubic cell= (\frac{4(0.128*10^{-9}}{\sqrt{2}})^3

Volume of face centered cubic cell=4.74531*10^{-29} m^3

3 0
4 years ago
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