Thermodynamics: An Engineering Approach ( 9th International Edition ) ISBN:9781260092684
Thermodynamics: An Engineering Approach ( 9th International Edition ) ISBN:9781260092684
9th Edition
ISBN: 9781260048667
Author: Yunus A. Cengel Dr.; Michael A. Boles
Publisher: McGraw-Hill Education
bartleby

Videos

Question
Book Icon
Chapter 17.7, Problem 122RP
To determine

To derive an expression for the speed of sound based on van der Walls’s equation of state P=RTvbav2 and using this relation determine the speed of sound in carbon dioxide at 80°C and 320kPa, and compare the result to that obtained by assuming ideal-gas behavior.

Expert Solution & Answer
Check Mark

Answer to Problem 122RP

The speed of sound in carbon dioxide by using the relation obtained from the van der Walls equation is 289.43m/s.

The speed of sound in carbon dioxide by assuming as ideal gas is 292.04m/s.

Explanation of Solution

Write the given equation of state.

P=RTvbav2 (I)

Here, the pressure is P, the gas constant is R, the temperature is T, the specific volume is v, and the van der Walls constants are a,b.

Partially differentiate the Equation (I) with respect to specific volume v by the keeping the temperature T as constant.

(Pv)T=v(RTvbav2)T=v(RTvb)Tv(av2)T=RTv(1vb)av(1v2)=RT[1(vb)2]a(2v3)

=RT(vb)2+2av3 (II)

Write the relation of speed of the sound.

c2=k(Pρ)T (III)

Here, the specific heat ratio is k, the pressure is P, the density is ρ, and the symbol indicates the partial derivative of variables.

Write the relation between density and specific volume.

ρ=1v

Partially differentiate the ρ with respect to specific volume v.

ρv=v(1v)ρv=1v2ρ=v(1v2)ρ=vv2

Substitute vv2 for ρ in Equation (III).

c2=k(Pvv2)T=kv2(Pv)T (IV)

Substitute RT(vb)2+2av3 for (Pv)T in Equation (IV).

c2=kv2[RT(vb)2+2av3]=(kv2)RT(vb)2+(kv2)2av3=v2kRT(vb)22akv (V)

Write the formula for velocity of sound at the given conditions of CO2 by assuming it as ideal gas.

c=kRT (VI)

Refer Table A-1, “Molar mass, gas constant, and critical-point properties”.

The molar mass (M) of carbon dioxide is 44.01kg/kmol44kg/kmol.

The gas constant (R) of carbon dioxide is 0.1889kJ/kgK or 0.1889kPam3/kgK.

Refer Table A-2, “Ideal-gas specific heats of various common gases”.

The specific heat ratio (k) of carbon dioxide is 1.289.

Conclusion:

Express the van der Walls constant a and b per unit mass as follows.

a=364.3kPam6/kmol2×1(44kg/kmol)2=364.3kPam6/kmol21936kg2/kmol2=0.1882kPam6/kg2

b=0.0427m3/kmol×144kg/kmol=9.70×104m3/kg

Substitute 320kPa for P, 0.1889kPam3/kgK for R, 80°C for T, 9.70×104m3/kg for b, and 0.1882kPam6/kg2 for a in Equation (I).

320kPa=(0.1889kPam3/kgK)(80°C)v9.70×104m3/kg0.1882kPam6/kg2v2320kPa=(0.1889kPam3/kgK)(80+273)Kv0.00097m3/kg0.1882kPam6/kg2v2320kPa=66.6817kPam3/kgv0.00097m3/kg0.1882kPam6/kg2v2 (VII)

By using Equation solver or online calculator solve the Equation (VII) and the value of v is obtained as follows.

v=0.2065m3/kg

Substitute 0.2065m3/kg for v, 1.279 for k, 0.1889kPam3/kgK for R, 80°C for T, 9.70×104m3/kg for b, and 0.1882kPam6/kg2 for a in Equation (V).

c2=[(0.2065m3/kg)2(1.279)(0.1889kPam3/kgK)(80°C)(0.2065m3/kg9.70×104m3/kg)22(0.1882kPam6/kg2)(1.279)0.2065m3/kg]c2=[(0.05454m6/kg2)(0.1889kPam3/kgK)(80+273)K0.04224m6/kg22.3313kPam3/kg]c2=[(0.05454m6/kg2)(66.6817kPam3/kg)0.04224m6/kg22.3313kPam3/kg]c2=86.0989kPam3/kg2.3313kPam3/kg

c2=83.7676kPam3/kg×1000m2/s21kPam3/kgc=83767.6m2/s2c=289.4263m/s289.43m/s

Thus, the speed of sound in carbon dioxide by using the relation obtained from the van der Walls equation is 289.43m/s.

When the carbon dioxide is assumed as ideal gas, the velocity of sound is determined as follows.

Substitute 0.1889kJ/kgK for R, 1.279 for k, and 80°C for T in Equation (VI).

c=1.279×0.1889kJ/kgK×80°C=1.279×0.1889kJ/kgK×(80+273)K=85.2859kJ/kg×1000m2/s21kJ/kg=292.0375m/s

292.04m/s

Thus, the speed of sound in carbon dioxide by assuming as ideal gas is 292.04m/s.

Want to see more full solutions like this?

Subscribe now to access step-by-step solutions to millions of textbook problems written by subject matter experts!
Students have asked these similar questions
Q Derive (continuity equation)? I want to derive clear mathematics.
motor supplies 200 kW at 6 Hz to flange A of the shaft shown in Figure. Gear B transfers 125 W of power to operating machinery in the factory, and the remaining power in the shaft is mansferred by gear D. Shafts (1) and (2) are solid aluminum (G = 28 GPa) shafts that have the same diameter and an allowable shear stress of t= 40 MPa. Shaft (3) is a solid steel (G = 80 GPa) shaft with an allowable shear stress of t = 55 MPa. Determine: a) the minimum permissible diameter for aluminum shafts (1) and (2) b) the minimum permissible diameter for steel shaft (3). c) the rotation angle of gear D with respect to flange A if the shafts have the minimum permissible diameters as determined in (a) and (b).
First monthly exam Gas dynamics Third stage Q1/Water at 15° C flow through a 300 mm diameter riveted steel pipe, E-3 mm with a head loss of 6 m in 300 m length. Determine the flow rate in pipe. Use moody chart. Q2/ Assume a car's exhaust system can be approximated as 14 ft long and 0.125 ft-diameter cast-iron pipe ( = 0.00085 ft) with the equivalent of (6) regular 90° flanged elbows (KL = 0.3) and a muffler. The muffler acts as a resistor with a loss coefficient of KL= 8.5. Determine the pressure at the beginning of the exhaust system (pl) if the flowrate is 0.10 cfs, and the exhaust has the same properties as air.(p = 1.74 × 10-3 slug/ft³, u= 4.7 x 10-7 lb.s/ft²) Use moody chart (1) MIDAS Kel=0.3 Q3/Liquid ammonia at -20°C is flowing through a 30 m long section of a 5 mm diameter copper tube(e = 1.5 × 10-6 m) at a rate of 0.15 kg/s. Determine the pressure drop and the head losses. .μ= 2.36 × 10-4 kg/m.s)p = 665.1 kg/m³

Chapter 17 Solutions

Thermodynamics: An Engineering Approach ( 9th International Edition ) ISBN:9781260092684

Ch. 17.7 - Prob. 11PCh. 17.7 - Prob. 12PCh. 17.7 - Prob. 13PCh. 17.7 - Prob. 14PCh. 17.7 - Prob. 15PCh. 17.7 - Prob. 16PCh. 17.7 - Prob. 17PCh. 17.7 - Prob. 18PCh. 17.7 - Prob. 19PCh. 17.7 - Prob. 20PCh. 17.7 - Prob. 21PCh. 17.7 - Prob. 22PCh. 17.7 - Prob. 23PCh. 17.7 - Prob. 24PCh. 17.7 - Prob. 25PCh. 17.7 - Prob. 26PCh. 17.7 - The isentropic process for an ideal gas is...Ch. 17.7 - Is it possible to accelerate a gas to a supersonic...Ch. 17.7 - Prob. 29PCh. 17.7 - Prob. 30PCh. 17.7 - A gas initially at a supersonic velocity enters an...Ch. 17.7 - Prob. 32PCh. 17.7 - Prob. 33PCh. 17.7 - Prob. 34PCh. 17.7 - Prob. 35PCh. 17.7 - Prob. 36PCh. 17.7 - Prob. 37PCh. 17.7 - Air at 25 psia, 320F, and Mach number Ma = 0.7...Ch. 17.7 - Prob. 39PCh. 17.7 - Prob. 40PCh. 17.7 - Prob. 41PCh. 17.7 - Prob. 42PCh. 17.7 - Prob. 43PCh. 17.7 - Is it possible to accelerate a fluid to supersonic...Ch. 17.7 - Prob. 45PCh. 17.7 - Prob. 46PCh. 17.7 - Prob. 47PCh. 17.7 - Consider subsonic flow in a converging nozzle with...Ch. 17.7 - Consider a converging nozzle and a...Ch. 17.7 - Prob. 50PCh. 17.7 - Prob. 51PCh. 17.7 - Prob. 52PCh. 17.7 - Prob. 53PCh. 17.7 - Prob. 54PCh. 17.7 - Prob. 57PCh. 17.7 - Prob. 58PCh. 17.7 - Prob. 59PCh. 17.7 - Prob. 60PCh. 17.7 - Prob. 61PCh. 17.7 - Air enters a nozzle at 0.5 MPa, 420 K, and a...Ch. 17.7 - Prob. 63PCh. 17.7 - Are the isentropic relations of ideal gases...Ch. 17.7 - What do the states on the Fanno line and the...Ch. 17.7 - It is claimed that an oblique shock can be...Ch. 17.7 - Prob. 69PCh. 17.7 - Prob. 70PCh. 17.7 - For an oblique shock to occur, does the upstream...Ch. 17.7 - Prob. 72PCh. 17.7 - Prob. 73PCh. 17.7 - Prob. 74PCh. 17.7 - Prob. 75PCh. 17.7 - Prob. 76PCh. 17.7 - Prob. 77PCh. 17.7 - Prob. 78PCh. 17.7 - Prob. 79PCh. 17.7 - Air flowing steadily in a nozzle experiences a...Ch. 17.7 - Air enters a convergingdiverging nozzle of a...Ch. 17.7 - Prob. 84PCh. 17.7 - Prob. 85PCh. 17.7 - Consider the supersonic flow of air at upstream...Ch. 17.7 - Prob. 87PCh. 17.7 - Prob. 88PCh. 17.7 - Air flowing at 40 kPa, 210 K, and a Mach number of...Ch. 17.7 - Prob. 90PCh. 17.7 - Prob. 91PCh. 17.7 - Prob. 92PCh. 17.7 - What is the characteristic aspect of Rayleigh...Ch. 17.7 - Prob. 94PCh. 17.7 - Prob. 95PCh. 17.7 - What is the effect of heat gain and heat loss on...Ch. 17.7 - Consider subsonic Rayleigh flow of air with a Mach...Ch. 17.7 - Prob. 98PCh. 17.7 - Prob. 99PCh. 17.7 - Air is heated as it flows subsonically through a...Ch. 17.7 - Prob. 101PCh. 17.7 - Prob. 102PCh. 17.7 - Prob. 103PCh. 17.7 - Air enters a rectangular duct at T1 = 300 K, P1 =...Ch. 17.7 - Prob. 106PCh. 17.7 - Prob. 107PCh. 17.7 - Air is heated as it flows through a 6 in 6 in...Ch. 17.7 - What is supersaturation? Under what conditions...Ch. 17.7 - Steam enters a converging nozzle at 5.0 MPa and...Ch. 17.7 - Steam enters a convergingdiverging nozzle at 1 MPa...Ch. 17.7 - Prob. 112PCh. 17.7 - Prob. 113RPCh. 17.7 - Prob. 114RPCh. 17.7 - Prob. 115RPCh. 17.7 - Prob. 116RPCh. 17.7 - Prob. 118RPCh. 17.7 - Prob. 119RPCh. 17.7 - Using Eqs. 174, 1713, and 1714, verify that for...Ch. 17.7 - Prob. 121RPCh. 17.7 - Prob. 122RPCh. 17.7 - Prob. 123RPCh. 17.7 - Prob. 124RPCh. 17.7 - Prob. 125RPCh. 17.7 - Prob. 126RPCh. 17.7 - Nitrogen enters a convergingdiverging nozzle at...Ch. 17.7 - An aircraft flies with a Mach number Ma1 = 0.9 at...Ch. 17.7 - Prob. 129RPCh. 17.7 - Helium expands in a nozzle from 220 psia, 740 R,...Ch. 17.7 - Helium expands in a nozzle from 0.8 MPa, 500 K,...Ch. 17.7 - Air is heated as it flows subsonically through a...Ch. 17.7 - Air is heated as it flows subsonically through a...Ch. 17.7 - Prob. 134RPCh. 17.7 - Prob. 135RPCh. 17.7 - Air is cooled as it flows through a 30-cm-diameter...Ch. 17.7 - Saturated steam enters a convergingdiverging...Ch. 17.7 - Prob. 138RPCh. 17.7 - Prob. 145FEPCh. 17.7 - Prob. 146FEPCh. 17.7 - Prob. 147FEPCh. 17.7 - Prob. 148FEPCh. 17.7 - Prob. 149FEPCh. 17.7 - Prob. 150FEPCh. 17.7 - Prob. 151FEPCh. 17.7 - Prob. 152FEPCh. 17.7 - Consider gas flow through a convergingdiverging...Ch. 17.7 - Combustion gases with k = 1.33 enter a converging...
Knowledge Booster
Background pattern image
Mechanical Engineering
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.
Similar questions
SEE MORE QUESTIONS
Recommended textbooks for you
Text book image
Elements Of Electromagnetics
Mechanical Engineering
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Oxford University Press
Text book image
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:9780134319650
Author:Russell C. Hibbeler
Publisher:PEARSON
Text book image
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:9781259822674
Author:Yunus A. Cengel Dr., Michael A. Boles
Publisher:McGraw-Hill Education
Text book image
Control Systems Engineering
Mechanical Engineering
ISBN:9781118170519
Author:Norman S. Nise
Publisher:WILEY
Text book image
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Cengage Learning
Text book image
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:9781118807330
Author:James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:WILEY
Intro to Compressible Flows — Lesson 1; Author: Ansys Learning;https://www.youtube.com/watch?v=OgR6j8TzA5Y;License: Standard Youtube License