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Resolução dos livros de mecanica dos fluidos, edição 7, ate o capitulo 6.
Tipologia: Exercícios
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1.1 A number of common substances are Tar Sand ‘‘Silly Putty’’ Jello Modeling clay Toothpaste Wax Shaving cream Some of these materials exhibit characteristics of both solid and fluid behavior under different conditions. Explain and give examples.
Tar Sand “Silly Putty” Jello Modeling clay Toothpaste Wax Shaving cream Some of these substances exhibit characteristics of solids and fluids under different conditions.
pressures or over long periods, they exhibit fluid characteristics. At higher temperatures, all three liquefy and become viscous fluids. Modeling clay and silly putty show fluid behavior when sheared slowly. However, they fracture under suddenly applied stress, which is a characteristic of solids. Toothpaste behaves as a solid when at rest in the tube. When the tube is squeezed hard, toothpaste “flows” out the spout, showing fluid behavior. Shaving cream behaves similarly. Sand acts solid when in repose (a sand “pile”). However, it “flows” from a spout or down a steep incline.
1.3 Discuss the physics of skipping a stone across the water surface of a lake. Compare these mechanisms with a stone as it bounces after being thrown along a roadway.
Open-Ended Problem Statement: Consider the physics of “skipping” a stone across the water surface of a lake. Compare these mechanisms with a stone as it bounces after being thrown along a roadway. Discussion: Observation and experience suggest two behaviors when a stone is thrown along a water surface:
1.4 The barrel of a bicycle tire pump becomes quite warm during use. Explain the mechanisms responsible for the temperature increase.
Open-Ended Problem Statement: The barrel of a bicycle tire pump becomes quite warm during use. Explain the mechanisms responsible for the temperature increase. Discussion: Two phenomena are responsible for the temperature increase: (1) friction between the pump piston and barrel and (2) temperature rise of the air as it is compressed in the pump barrel. Friction between the pump piston and barrel converts mechanical energy (force on the piston moving through a distance) into thermal energy as a result of friction. Lubricating the piston helps to provide a good seal with the pump barrel and reduces friction (and therefore force) between the piston and barrel. Temperature of the trapped air rises as it is compressed. The compression is not adiabatic because it occurs during a finite time interval. Heat is transferred from the warm compressed air in the pump barrel to the cooler surroundings. This raises the temperature of the barrel, making its outside surface warm (or even hot!) to the touch.
Basic equation: (^) ρ (^) Rp = air ⋅T
Given or available data (^) p = 14.7psi T = ( 59 + 460 )R Rair =53.33 ⋅ lbm Rft lbf⋅⋅
V = 10 ft⋅ × 10 ⋅ ft× 8 ⋅ft V =800 ft 3
Then (^) ρ (^) Rp = (^) air ⋅T ρ 0. lbm ft 3
= ρ 0.00238 slug ft 3
= ρ 1.23 kg m 3
M = ρ ⋅V M = 61.2 lbm M = 1.90 slug M =27.8 kg
The given or available data is: (^) M = 10 lbm⋅ p = ( 200 + 1 ) atm⋅ p =2.95 × 10 3 ⋅psi
T = ( 70 + 460 ) K⋅ T = 954 R⋅ RN2 = 55.16 ⋅ lbm Rft lbf⋅⋅ (Table A.6)
The governing equation is the ideal gas equation (^) p = ρ ⋅R (^) N2⋅T and (^) ρ =MV
where V is the tank volume (^) V π^ D^
= 4 ⋅L where^ L =2 D⋅
Combining these equations:
Hence (^) M = V⋅ ρ Rp V⋅ = (^) N2 ⋅T p RN2 ⋅T
π ⋅D^2 = ⋅ 4 ⋅L p RN2 ⋅T
π ⋅D^2 = ⋅ 4 ⋅ 2 ⋅D p ⋅π ⋅D^3 = 2 R⋅ (^) N2⋅T
1 3 = D (^) π^2 × 55.16⋅ (^) lbm Rft lbf⋅⋅ × 954 ⋅ K× 10 ⋅ lbm × 29501 in
2 ⋅ (^) lbf ft 12 in⋅
2
1 3 =
D = 1.12 ft⋅ D = 13.5 in⋅ L = 2 D⋅ L =27 in⋅
These are internal dimensions; the external ones are 1/4 in. larger: L = 27.25 in⋅ D =13.75 in⋅
or (^1) W kV e V Wk 1
kgtW kgtW − = = L− N
MM O Q
− (^) ; e− PP
But V→V (^) t as t→∞, so Vt = Wk. Therefore (^) VVt 1 e
kgtW = − −
When (^) VVt= 0.95, then e 0. −kgtW = and kgtW = 3. Thus t = 3 W/gk
1.9 Consider again the small particle of Problem 1.8. Express the distance required to reach 95 percent of its terminal speed in terms of g , k , and W.
V is speed.
Basic equation: ∑F y = ma y Assumptions:
Then, (^) ∑ F y (^) = W − kV = ma (^) y = m dVdt =Wg VdVdy or 1 − (^) Wk V=V dVg dy
Separating variables V^1 t
Integrating, noting that velocity is zero initially
[ ]
0.95 0. 2 (^00)
2 2 2 2 2 2 2 2
Vt V^ t t t t t t t t t t t
∫
Using the given data
0 0.01 0.
The time to reach 95% of maximum speed is obtained from (^3) ⋅M gπ ⋅⋅ μ⋅ d 1 e
− 3 ⋅ π⋅ μ⋅d
The plot can also be done in Excel.
The data provided, or available in the Appendices, are:
μ 1.8 × 10 −^5 N s⋅ m^2
= ⋅ ρw 999 kg m^3
= ⋅ SGgas = 0.72 ρgas = SGgas ⋅ρw ρgas 719 kg m^3
Newton's 2nd law for the sphere (mass M) is (ignoring buoyancy effects) (^) M ⋅ dVdt =M g⋅ − 3 ⋅ π⋅μ ⋅V ⋅d
so dV g −^3 ⋅π^ M⋅^ μ ⋅d⋅V
= dt
Integrating and using limits (^) V t( ) (^3) ⋅ M gπ⋅⋅μ ⋅d 1 e
− 3 ⋅ π⋅ μ⋅d
Integrating again (^) x t( ) (^3) ⋅M g π⋅⋅μ ⋅d t (^3) ⋅ πM⋅μ ⋅d e
− 3 ⋅ π⋅ μ⋅d
Replacing M with an expression involving diameter d (^) M ρgas^ π^ d
= ⋅ 6 x t( ) ρgas ⋅ d 2 ⋅g 18 ⋅μ t
ρgas ⋅d 2 18 ⋅μ e
− 18 ⋅μ ρgas ⋅d^2 ⋅^ t− 1
This equation must be solved for d so that x 1 s( ⋅) = 1 m⋅. The answer can be obtained from manual iteration, or by using Excel's Goal Seek. (See this in the corresponding Excel workbook.)
d =0.109 mm⋅
0 0.2 0.4 0.6 0.8 1
Note That the particle quickly reaches terminal speed, so that a simpler approximate solution would be to solve Mg = 3πμ Vd for d , with V = 0.25 m/s (allowing for the fact that M is a function of d )!
0 100 200 300 400 500
20
40
60
(c) For V ( t ) we need to integrate (1) with respect to t : M ⋅ dVdt =M g⋅ −k V ⋅ 2
Separating variables and integrating:
0
V M g⋅V V k V^
d 0
t =^ ⌠⎮⌡ 1 dt
so t 12 ⋅ (^) k gM⋅ ln
M g⋅ k +V M g⋅ k −V
= ⋅^12 ⋅ (^) k gM⋅ ln V Vt^ +V t −V
Rearranging V t( ) Vt e
2 ⋅ k g M⋅ ⋅t − 1
e
2 ⋅ k g M⋅ ⋅t
0 5 10 15 20
20
40
60
V t( )
t
The two graphs can also be plotted in Excel.
m 2
= ⋅ khoriz 0.05 N s
m 2
= ⋅ U 0 = 70 ⋅ms
Treat the sky diver as a system; apply Newton's 2nd law in horizontal and vertical directions:
Vertical: Newton's 2nd law for the sky diver (mass M) is (ignoring buoyancy effects): (^) M ⋅ dVdt = M g⋅ −kvert ⋅V 2 (1)
For V ( t ) we need to integrate (1) with respect to t :
Separating variables and integrating:
0
V M g⋅V V kvert V
d 0
t =^ ⌠⎮⌡ 1 dt
so (^) t (^12) kM ⋅ (^) vert ⋅gln
M g⋅ kvert+V M g⋅ kvert−V
Rearranging orV t( ) (^) kM g⋅ vert
e
2 ⋅ kvert M⋅g⋅t − 1
e
2 ⋅ kvert M⋅g⋅t
For y ( t ) we need to integrate again: dydt = V or (^) y =^ ⌠⎮⎮⌡ V dt
y t( ) 0
t =^ ⌠⎮⌡ V t( )dt 0
t
0 20 40 60
500
1 10 ×^3
1.5 10 × 3
2 10 ×^3
t
Plotting the trajectory:
0 1 2 3
− 3
− 2
− 1
These plots can also be done in Excel.
The data provided are: (^) M = 5 10⋅ −^11 ⋅kg Vt = 5 ⋅cms
Newton's 2nd law for the general motion is (ignoring buoyancy effects) (^) M ⋅ dVdt = M g⋅ −k V⋅ (1)
Newton's 2nd law for the steady state motion becomes (ignoring buoyancy effects) (^) M g⋅ = k V⋅ t so (^) k M g V⋅ = t
k = M g V⋅t 5 × 10 −^11 ⋅kg × 9.81m s^2
= ⋅ ×0.05 ms⋅ k =9.81 × 10 −^9 ⋅N s m⋅
dV g −M k⋅V To find the time to reach 99% of V (^) t , we need V ( t ). From 1, separating variables =^ dt
We must evaluate this when (^) V = 0.99 V⋅ t V =4.95 ⋅cms
t 5 × 10 −^11 ⋅ kg m 9.81 × 10 −^9 ⋅ N⋅s
× N s
× (^) kg m⋅ ln 1 9.81 10 ⋅ −^9 N s⋅ ⋅ (^) m
5 × 10 −^11 ⋅kg
× s
2 × (^) 9.81 m⋅ 0.0495 m⋅ × (^) s kg m⋅ N s ⋅^2
t =0.0235 s