FLUID MECHANICS FUNDAMENTALS+APPS
FLUID MECHANICS FUNDAMENTALS+APPS
4th Edition
ISBN: 2810022150991
Author: CENGEL
Publisher: MCG
bartleby

Videos

Question
Book Icon
Chapter 12, Problem 148P
To determine

To plot: the mass flow parameter.

Expert Solution & Answer
Check Mark

Answer to Problem 148P

FLUID MECHANICS FUNDAMENTALS+APPS, Chapter 12, Problem 148P , additional homework tip  1

Explanation of Solution

Given:

Mach number k=1.2,1.4 and 1.6 range of 0Ma1.

Calculation:

Equation is given by

  m. R T 0 AP0=PAMa k RT R T 0 AP0m. R T 0 AP0=Mak(P P 0 )( T 0 T )m. R T 0 AP0=Mak( ( 1+ k-1 2 M a 2 ) -k/k-1)(1+ k-1 2M a 2)1/2m. R T 0 AP0=Mak( ( 1+ k-1 2 M a 2 ) -( k+1 )/2( k-1 ))

  k=1.4Ma=0.2m. R T 0 AP0=0.21.4( ( 1+ 1.4-1 2 0. 2 2 ) -( 1.4+1 )/2( 1.4-1 ))m. R T 0 AP0=0.231

  k=1.4Ma=0.4m. R T 0 AP0=0.41.4( ( 1+ 1.4-1 2 0. 4 2 ) -( 1.4+1 )/2( 1.4-1 ))m. R T 0 AP0=0.4306

  k=1.4Ma=0.6m. R T 0 AP0=0.61.4( ( 1+ 1.4-1 2 0. 6 2 ) -( 1.4+1 )/2( 1.4-1 ))m. R T 0 AP0=0.57

  k=1.4Ma=0.8m. R T 0 AP0=0.81.4( ( 1+ 1.4-1 2 0. 8 2 ) -( 1.4+1 )/2( 1.4-1 ))m. R T 0 AP0=0.65

  k=1.4Ma=1.0m. R T 0 AP0=1.01.4( ( 1+ 1.4-1 2 1. 0 2 ) -( 1.4+1 )/2( 1.4-1 ))m. R T 0 AP0=0.68

  k=1.6Ma=0.2m. R T 0 AP0=0.21.6( ( 1+ 1.6-1 2 0. 2 2 ) -( 1.6+1 )/2( 1.6-1 ))m. R T 0 AP0=0.246

  k=1.6Ma=0.4m. R T 0 AP0=0.41.6( ( 1+ 1.6-1 2 0. 4 2 ) -( 1.6+1 )/2( 1.6-1 ))m. R T 0 AP0=0.457

  k=1.6Ma=0.6m. R T 0 AP0=0.61.6( ( 1+ 1.6-1 2 0. 6 2 ) -( 1.6+1 )/2( 1.6-1 ))m. R T 0 AP0=0.607

  k=1.6Ma=0.8m. R T 0 AP0=0.81.6( ( 1+ 1.6-1 2 0. 8 2 ) -( 1.6+1 )/2( 1.6-1 ))m. R T 0 AP0=0.69

  k=1.6Ma=1.0m. R T 0 AP0=1.01.6( ( 1+ 1.6-1 2 1. 0 2 ) -( 1.6+1 )/2( 1.6-1 ))m. R T 0 AP0=0.71

  k=1.2Ma=0.2m. R T 0 AP0=0.21.2( ( 1+ 1.2-1 2 0. 2 2 ) -( 1.2+1 )/2( 1.2-1 ))m. R T 0 AP0=0.214

  k=1.2Ma=0.4m. R T 0 AP0=0.41.2( ( 1+ 1.2-1 2 0. 4 2 ) -( 1.2+1 )/2( 1.2-1 ))m. R T 0 AP0=0.401

  k=1.2Ma=0.6m. R T 0 AP0=0.61.2( ( 1+ 1.2-1 2 0. 6 2 ) -( 1.2+1 )/2( 1.2-1 ))m. R T 0 AP0=0.541

  k=1.2Ma=0.8m. R T 0 AP0=0.81.2( ( 1+ 1.2-1 2 0. 8 2 ) -( 1.2+1 )/2( 1.2-1 ))m. R T 0 AP0=0.62

  k=1.2Ma=1.0m. R T 0 AP0=1.01.2( ( 1+ 1.2-1 2 1. 0 2 ) -( 1.2+1 )/2( 1.2-1 ))m. R T 0 AP0=0.64

The graph for the above values is given below:

FLUID MECHANICS FUNDAMENTALS+APPS, Chapter 12, Problem 148P , additional homework tip  2

Conclusion:

Therefore, for the values Ma and k are plotted but only one value of k and Ma.

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
FIGURE P1.37 1.38 WP As shown in Figure P1.38, an inclined manometer is used to measure the pressure of the gas within the reservoir, (a) Using data on the figure, determine the gas pressure, in lbf/in.² (b) Express the pressure as a gage or a vacuum pressure, as appropriate, in lbf/in.² (c) What advantage does an inclined manometer have over the U-tube manometer shown in Figure 1.7? Patm = 14.7 lbf/in.² L I C i Gas a Oil (p = 54.2 lb/ft³) 140° 8=32.2 ft/s² 15 in.
what is an low pressure Heater, what are formulas, and their importance, define the diagram, and give me a script on how to explain the design of an air preheater, and how did values end up in that number. based on standards
what is an air preheater, what are formulas, and their importance, define the diagram, and give me a script on how to explain the design of an air preheater, and how did values end up in that number. based on standards

Chapter 12 Solutions

FLUID MECHANICS FUNDAMENTALS+APPS

Ch. 12 - Prob. 74PCh. 12 - Prob. 75PCh. 12 - For an ideal gas flowing through a normal shock,...Ch. 12 - Prob. 77CPCh. 12 - On a T-s diagram of Raleigh flow, what do the...Ch. 12 - What is the effect of heat gain and heat toss on...Ch. 12 - Prob. 80CPCh. 12 - Prob. 81CPCh. 12 - Prob. 82CPCh. 12 - Argon gas enters a constant cross-sectional area...Ch. 12 - Prob. 84EPCh. 12 - Prob. 85PCh. 12 - Prob. 86PCh. 12 - Prob. 87EPCh. 12 - Prob. 88PCh. 12 - Prob. 89PCh. 12 - Prob. 90PCh. 12 - Prob. 91PCh. 12 - Prob. 93CPCh. 12 - Prob. 94CPCh. 12 - Prob. 95CPCh. 12 - Prob. 96CPCh. 12 - Prob. 97CPCh. 12 - Prob. 98CPCh. 12 - Prob. 99CPCh. 12 - Prob. 100CPCh. 12 - Prob. 101PCh. 12 - Air enters a 5-cm-diameter, 4-m-long adiabatic...Ch. 12 - Helium gas with k=1.667 enters a 6-in-diameter...Ch. 12 - Air enters a 12-cm-diameter adiabatic duct at...Ch. 12 - Prob. 105PCh. 12 - Air flows through a 6-in-diameter, 50-ft-long...Ch. 12 - Air in a room at T0=300k and P0=100kPa is drawn...Ch. 12 - Prob. 110PCh. 12 - Prob. 112PCh. 12 - Prob. 113PCh. 12 - Prob. 114PCh. 12 - Prob. 115PCh. 12 - Prob. 116EPCh. 12 - A subsonic airplane is flying at a 5000-m altitude...Ch. 12 - Prob. 118PCh. 12 - Prob. 119PCh. 12 - Prob. 120PCh. 12 - Prob. 121PCh. 12 - Prob. 122PCh. 12 - Prob. 123PCh. 12 - An aircraft flies with a Mach number Ma1=0.9 at an...Ch. 12 - Prob. 125PCh. 12 - Helium expands in a nozzle from 220 psia, 740 R,...Ch. 12 - Prob. 127PCh. 12 - Prob. 128PCh. 12 - Prob. 129PCh. 12 - Prob. 130PCh. 12 - Prob. 131PCh. 12 - Prob. 132PCh. 12 - Prob. 133PCh. 12 - Prob. 134PCh. 12 - Prob. 135PCh. 12 - Prob. 136PCh. 12 - Prob. 137PCh. 12 - Prob. 138PCh. 12 - Air is cooled as it flows through a 30-cm-diameter...Ch. 12 - Prob. 140PCh. 12 - Prob. 141PCh. 12 - Prob. 142PCh. 12 - Prob. 145PCh. 12 - Prob. 148PCh. 12 - Prob. 149PCh. 12 - Prob. 150PCh. 12 - Prob. 151PCh. 12 - Prob. 153PCh. 12 - Prob. 154PCh. 12 - Prob. 155PCh. 12 - Prob. 156PCh. 12 - Prob. 157PCh. 12 - Prob. 158PCh. 12 - Prob. 159PCh. 12 - Prob. 160PCh. 12 - Prob. 161PCh. 12 - Prob. 162PCh. 12 - Assuming you have a thermometer and a device to...
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