Theory and Design for Mechanical Measurements
6th Edition
ISBN: 9781118881279
Author: Richard S. Figliola, Donald E. Beasley
Publisher: WILEY
expand_more
expand_more
format_list_bulleted
Videos
Textbook Question
Chapter 9, Problem 9.25P
The pressure transmission line response equation of Equation 9.23 can also be derived by considering the forces acting on a fluid element within the connecting tubing (12). Develop a model for the system measured pressure response based on an applied pressure force, shear resistance force, and restoring compliance related force through Newton’s momentum (second law) principles. Refer to Figure 9.35.
Figure 9.35 Freebody diagram on a fluid element (x-direction) for Problem 9.25.
Expert Solution & Answer
Want to see the full answer?
Check out a sample textbook solution
Students have asked these similar questions
1. Aspring mass system serving as a shock absorber under a car s suspension, supports the
M = 1000 kg mass or the car. For this shock absorber,
k = 1x 10°/m and c = 2x 10' N s/m. Tne car drives over a corrugated road with rorce
F = 2x 10' sin(@t) N. Use your notes to model the second order difrerential equation suited to this
application. Simplity the equation with the coerricient of X" as one. Soive X (tne general solution) in
terms or @ using the complimentary and particular solution method. In determining the coernicients of
your particular solution, it will be required that you assume o -1xo or 1- w x -m. Do not
use Matiab as its solution will not be identiriable in the solution entry. Do not determine the value of W.
You must Indicate In your solution!
1. Tne simpliried dirrerential equation in terms or the displacement X you will be solving
2. Ine m equation and complimentary solution Xe
3. Tne choice ror the particular solution and the actual particular solution Xp
4. Express…
part 3 4 and 5 please of this question
With reference to the attached example.
Apply dimensinal analysis to show that all values/units used are homogeneous.
Chapter 9 Solutions
Theory and Design for Mechanical Measurements
Ch. 9 - Prob. 9.1PCh. 9 - 9.2 State the following pressures as absolute...Ch. 9 - A water-filled manometer is used to measure the...Ch. 9 - Prob. 9.4PCh. 9 - 9.5 The pressure differential across an orifice...Ch. 9 - Show that the static sensitivity of an inclined...Ch. 9 - Prob. 9.7PCh. 9 - Show that the instrument (systematic) uncertainty...Ch. 9 - A strain gauge, diaphragm pressure transducer...Ch. 9 - Select a practical fluid to use in a manometer to...
Ch. 9 - An air pressure over the 200- to 400-N/m2 range is...Ch. 9 - Calculate the design-stage uncertainty in...Ch. 9 - The pressure drop across a valve through which air...Ch. 9 - Estimate the sensitivity (pF/mm) of a capacitance...Ch. 9 - A diaphragm pressure transducer is calibrated...Ch. 9 - A diaphragm pressure transducer is coupled with a...Ch. 9 - Prob. 9.17PCh. 9 - A 2.0 mm thick circular steel diaphragm (Em = 200...Ch. 9 - Estimate the differential pressure limit for a...Ch. 9 - The pressure fluctuations in a pipe filled with...Ch. 9 - What is the sensitivity of a pitot-static tube...Ch. 9 - A pitot-static pressure probe inserted within a...Ch. 9 - A tall pitot-static tube is mounted through and...Ch. 9 - The pressure transmission line response equation...Ch. 9 - Prob. 9.26PCh. 9 - Prob. 9.28PCh. 9 - Compare the inertance of water in a 0.2-m-long...Ch. 9 - The output from a resting healthy human adult...Ch. 9 - Prob. 9.31PCh. 9 - A pressure drop of 213 Pa is measured between two...Ch. 9 - Wall pressure taps (e.g., Figs. 9.19 and 9.21) are...Ch. 9 - Prob. 9.34PCh. 9 - Prob. 9.35PCh. 9 - Determine the resolution of a manometer required...Ch. 9 - A long cylinder is placed into a wind tunnel and...Ch. 9 - Prob. 9.38PCh. 9 - Prob. 9.39PCh. 9 - What is the sound pressure in pascals if the...Ch. 9 - A 6-mm-diameter pitot-static tube is used as a...Ch. 9 - For the thermal anemometer in Figures 9.31 and...Ch. 9 - Determine the static sensitivity of the output...Ch. 9 - A laser Doppler anemometer setup in a dual-beam...Ch. 9 - A set of 5,000 measurements of velocity at a point...Ch. 9 - Aircraft airspeed is measured using a pitot...
Knowledge Booster
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
- the title of the book: Engineering Thermofluids Thermodynamics, Fluid Mechanics, and Heat Transfer by: Mahmoud Massoudarrow_forwardThe paragraph below contains more than one instance of false statements or incorrect logic. In a short answer (50 words or less) based on transport and mathematical concepts, describe at least two errors in this paragraph that leads to the faulty conclusion. Consider a gas confined within a large sealed holding tank. Assume that the gas is stagnant (in the continuum sense) so that v = Q everywhere inside the tank. The continuity equation Dp Dp -p(V.v) applies to this gas. Since v= Q the continuity equation reduces to = 0. Dt Dt Integrating this equation gives the result that the density of the gas must be constant at every position inside the tank. Constant density means the gas is incompressible. Since everyone knows gases are actually compressible, the original assumption that y = 0 must be incorrect. Thus, we conclude that it is not possible to have storage tanks full of stagnant gas – there must always be some non-zero velocity.arrow_forwardfluid mechanicsarrow_forward
- Air is compressed by a compressor in steady-state operation, i.e. the inlet mass flow rate qm is constant in time. The compressor is airtight. The area of the inlet and outlet cross-section is A and AOUT, respectively. The outlet-to-inlet density ratio is PouT PIN the outlet-to-inlet mass flow rate ratio is 9m-OUT/9m-IN- What is the outlet-to-inlet volume flow rate ratio? 9V-OUT/av-IN =? Select one: a. 9V-OUT/av-IN = (A OUT'A IN) (POUT PIN b. 9V-OUT/av-IN = PIN/POUT C. 9V-OUT/av-IN = 9m-OUT/ 9m-IN d. 9V-OUT/av-IN=AOUTAINarrow_forwardVibrationsarrow_forwardI need answer 2,3 and i give upvote (no plagarism)arrow_forward
- + a si diplacement #damping-Sear x dynamics systems questions 111 X Q V Highlight File C/Users/40332698/AppData/Local/Packages/microsoft windowscommunicationsapps_8wekyb3d8bbwe/LocalState/Files/50/145/Attachments/dynamics%... Page view A Read aloud | Add textDraw Q 8 of 40 a 2/59 At time t = 10 s, the velocity of a particle moving in the x-y plane is v= 0.1i+2j m/s. By time = 10.1 s, its velocity has become -0.1i + 1.8j m/s. Determine the magnitude aav of its average acceleration during this interval and the angle 0 made by the average accel- eration with the positive x-axis. Type here to search O H T JU E # 2 W S 3 E D C Ix $ R 5 T OL G F FO 6 Y H N & 7 U J 8 I K 9 prt sc O O L home P 1 + 11 To 1 Erase 12 E 9°C Cloudy Darrow_forwardConsider a pressure transducer connected to a pipe through a connecting tube of diameter 3.5 mm and a length of 50 mm. Water having viscosity 0.001 Pa.s is flowing in the pipe. There are pressure transients which occur every 7 seconds. The compliance of the pressure transducer is 25000000 mm³/bar. Calculate the time constant of the transducer in seconds.arrow_forwardPLEASE BOX YOUR ANSWERS Problem 2 In an experiment conducted in a laboratory, the surface tension (Y) acting on a rotating square plate in a viscous fluid is a function of the external torque (t), plate length (a), area moment of inertia of plate (I), specific weight of the fluid (Y) and angular displacement of the plate (0). Using Buckingham-Pi theorem, find a suitable set of pi terms (in M, L and T primary dimensions). Your final answer should be written in proper functional form. Refer Table 5.1/ page-296 for secondary dimension of the variables.arrow_forward
arrow_back_ios
SEE MORE QUESTIONS
arrow_forward_ios
Recommended textbooks for you
Elements Of ElectromagneticsMechanical EngineeringISBN:9780190698614Author:Sadiku, Matthew N. O.Publisher:Oxford University Press
Mechanics of Materials (10th Edition)Mechanical EngineeringISBN:9780134319650Author:Russell C. HibbelerPublisher:PEARSON
Thermodynamics: An Engineering ApproachMechanical EngineeringISBN:9781259822674Author:Yunus A. Cengel Dr., Michael A. BolesPublisher:McGraw-Hill Education
Control Systems EngineeringMechanical EngineeringISBN:9781118170519Author:Norman S. NisePublisher:WILEY
Mechanics of Materials (MindTap Course List)Mechanical EngineeringISBN:9781337093347Author:Barry J. Goodno, James M. GerePublisher:Cengage Learning
Engineering Mechanics: StaticsMechanical EngineeringISBN:9781118807330Author:James L. Meriam, L. G. Kraige, J. N. BoltonPublisher:WILEY
Elements Of Electromagnetics
Mechanical Engineering
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Oxford University Press
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:9780134319650
Author:Russell C. Hibbeler
Publisher:PEARSON
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:9781259822674
Author:Yunus A. Cengel Dr., Michael A. Boles
Publisher:McGraw-Hill Education
Control Systems Engineering
Mechanical Engineering
ISBN:9781118170519
Author:Norman S. Nise
Publisher:WILEY
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Cengage Learning
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:9781118807330
Author:James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:WILEY
Heat Transfer – Conduction, Convection and Radiation; Author: NG Science;https://www.youtube.com/watch?v=Me60Ti0E_rY;License: Standard youtube license