Problem 1.6 Make a guess at the order of magnitude of the mass (e.g., 0.01, 0.1, 1.0, 10, 100, or 1000 lbm or kg) of standard air that is in a room 10

Similar documents
UNIT CONVERSIONS User Guide & Disclaimer

Campus Mail Box. Circle One: Richards 03 Richards 04 Lui 05 Lui - 06

ES201 - Examination 2 Fall Instructor: NAME BOX NUMBER

The online of midterm-tests of Fluid Mechanics 1

CHAPTER 1 Basic Considerations

PUMP SYSTEM ANALYSIS AND SIZING. BY JACQUES CHAURETTE p. eng.

NEBB Fundamental Formulas

Applied Fluid Mechanics

Units and Dimensions. Lecture 1. Introduction to Chemical Engineering Calculations

Mechanical Engineering Department Third year class Gas Dynamics Tables Lecturer: Dr.Naseer Al-Janabi

Chapter 2 Dimensions, Units, and Unit Conversion

ME 201 Thermodynamics

CHAPTER 12 Turbomachinery

MOTOR WIRING DATA From National Electrical Code 3 PHASE SQUIRREL CAGE INDUCTION MOTORS 230 Volt 460 Volt Min. # Max. Rating

CHAPTER 1 Basic Considerations

SOLUTION MANUAL ENGLISH UNIT PROBLEMS CHAPTER 4 SONNTAG BORGNAKKE VAN WYLEN. FUNDAMENTALS of. Thermodynamics. Sixth Edition

Non-Newtonian fluids is the fluids in which shear stress is not directly proportional to deformation rate, such as toothpaste,

T m / A. Table C2 Submicroscopic Masses [2] Symbol Meaning Best Value Approximate Value

Basic Math Concepts for Water and Wastewater Operators. Daniel B. Stephens & Associates, Inc.

Problem Solving & Energy Balances 4: Those Pesky US Units ABET Course Outcomes: Important Resource: Class Plan distance Velocity time acceleration

CONCEPTS AND DEFINITIONS. Prepared by Engr. John Paul Timola

Table 10-T-11 : Alphabetical Listings of Common Conversions

Introduction to Mechanical Engineering Measurements Two Main Purposes of Measurements Engineering experimentation Operational systems

Chemical Engineering 374

Section 1: Theory of Heat Unit 2: Matter and Energy

DIMENSIONS AND UNITS

Learning Objectives. Lesson 6: Mathematical Models of Fluid Flow Components. ET 438a Automatic Control Systems Technology 8/27/2015

To receive full credit all work must be clearly provided. Please use units in all answers.

Northern Lesson 2 Gear Pump Terminology. Gear Pump 101. Lesson 2: Gear Pump Terminology. When your reputation depends on it!

Download Solution Manual for Thermodynamics for Engineers 1st Edition by Kroos and Potter

Chapter 2 Solutions. 2.1 (D) Pressure and temperature are dependent during phase change and independent when in a single phase.

Introduction to Mechanical Engineering

TOTAL HEAD, N.P.S.H. AND OTHER CALCULATION EXAMPLES Jacques Chaurette p. eng., June 2003

PART II. Fluid Mechanics Pressure. Fluid Mechanics Pressure. Fluid Mechanics Specific Gravity. Some applications of fluid mechanics

34.3. Resisted Motion. Introduction. Prerequisites. Learning Outcomes

CHAPTER 72 AREAS UNDER AND BETWEEN CURVES

Chapter 2 SOLUTION 100 = km = h. = h. ft s

Chapter 9b: Numerical Methods for Calculus and Differential Equations. Initial-Value Problems Euler Method Time-Step Independence MATLAB ODE Solvers

1. Metric system- developed in Europe (France) in 1700's, offered as an alternative to the British or English system of measurement.

CHARACTERISTIC OF FLUIDS. A fluid is defined as a substance that deforms continuously when acted on by a shearing stress at any magnitude.

CHAPTER 2: THE NATURE OF ENERGY

Chapter 5. Section 5.1. Section ( x ) ( y ) 7. ( x ) ( y ) (0, 3 + 5) and (0, 3 5)

1.4 Perform the following unit conversions: (b) (c) s. g s. lb min. (d) (e) in. ft s. m 55 h. (f) ft s. km h. (g)

ES201 - Examination 2 Winter Adams and Richards NAME BOX NUMBER

Annubar Primary Element Flow Calculations

ACCOUNTING FOR FRICTION IN THE BERNOULLI EQUATION FOR FLOW THROUGH PIPES

Metric prefixes and conversion constants

Summary of common Pressure Units Version 1.00, 12/15/2003

Conversion Factors COMMONLY USED CONVERSION FACTORS. Multiply By To Obtain

DIFFERENTIATION RULES

Non Newtonian Fluid Dynamics

2.0 KEY EQUATIONS. Evaporator Net Refrigeration Effect. Compressor Work. Net Condenser Effect

Unit Conversions, Important Constants and Relationships

Objectives. Power in Translational Systems 298 CHAPTER 6 POWER

2007 AP Calculus AB Free-Response Questions Section II, Part A (45 minutes) # of questions: 3 A graphing calculator may be used for this part

Chapter 1 INTRODUCTION

Fluid Properties and Units

PROPERTIES OF FLUIDS

FDE 211 MATERIAL & ENERGY BALANCES. Instructor: Dr. Ilgin Paker Yikici Fall 2015

G302 - Basics Review of Math and Algebra

Unit conversion problems, by Tony R. Kuphaldt (2006)

CHAPTER 1 INTRODUCTION

US Customary System (USC) Systeme Internationale (SI) Prefixes. Units & Significant Figures

KNOWN: Pressure, temperature, and velocity of steam entering a 1.6-cm-diameter pipe.

Practice Problems for Final Exam ENGR 120

MCE380: Measurements and Instrumentation Lab

Fluid Dynamics Exam #1: Introduction, fluid statics, and the Bernoulli equation March 2, 2016, 7:00 p.m. 8:40 p.m. in CE 118

ρ mixture = m mixture /V = (SG antifreeze ρ water V antifreeze + SG water ρ water V water )/V, so we get

2.000 Homework # 4: Machine components

EF 151 Final Exam, Fall, 2011 Page 1 of 11

1 centimeter (cm) 5 10 millimeters (mm) 1 meter (m) centimeters. 1 kilometer (km) 5 1,000 meters. Set up equivalent ratios and cross multiply.

FLOW MEASUREMENT IN PIPES EXPERIMENT

Course: TDEC202 (Energy II) dflwww.ece.drexel.edu/tdec

hp calculators HP 9g Solving Problems Involving Unit Conversions Metric Units and Imperial Units The CONV Menu

INTERNATIONAL SYSTEM OF UNITS

THE REALM OF PHYSICS AND MEASUREMENT HW/Study Packet

CHAPTER 3 BASIC EQUATIONS IN FLUID MECHANICS NOOR ALIZA AHMAD

Water Circuit Lab. The pressure drop along a straight pipe segment can be calculated using the following set of equations:

SEVENTH EDITION and EXPANDED SEVENTH EDITION

Name : Applied Physics II Exam One Winter Multiple Choice ( 7 Points ):

Only if handing in. Name: Student No.: Page 2 of 7

Solve the set of equations using the decomposition method and AX=B:

Chapter 1: INTRODUCTION AND BASIC CONCEPTS. Thermodynamics = Greek words : therme(heat) + dynamis(force or power)

1 1. Round off the following numbers to three significant figures: (a) m, (b) s, (c) 4555 N, and (d) 2768 kg.

ρg 998(9.81) LV 50 V. d2g 0.062(9.81)

Chapter 6. Losses due to Fluid Friction

Chapter 1 Dimensions, Units, and Their Conversion

Math 147 Exam II Practice Problems

APPENDIX B ABBREVIATIONS, SYMBOLS AND CONVERSION FACTORS Abbreviations

Universität Duisburg-Essen Fakultät für Ingenieurwissenschaften WS 2012 Maschinenbau, IVG, Thermodynamik Dr. M. A. Siddiqi

APPENDIX H CONVERSION FACTORS

CIVE HYDRAULIC ENGINEERING PART II Pierre Julien Colorado State University

INTRODUCTION DEFINITION OF FLUID. U p F FLUID IS A SUBSTANCE THAT CAN NOT SUPPORT SHEAR FORCES OF ANY MAGNITUDE WITHOUT CONTINUOUS DEFORMATION

PTAC: Applied Physics COURSE OUTLINE & OBJECTIVES ESC Approved October 8, 2004

Clicker Question Tune-up: This is much like physics!

Unit A-1: List of Subjects

CAE 331/513 Building Science Fall 2017

L = I ω = const. I = 2 3 MR2. When the balloon shrinks (because the air inside it cools down), the moment of inertia decreases, R = 1. L = I ω = I ω.

BAE 820 Physical Principles of Environmental Systems

CAE 331/513 Building Science Fall 2015

Transcription:

Problem 1.6 Make a guess at the order of magnitude of the mass (e.g., 0.01, 0.1, 1.0, 10, 100, or 1000 lbm or kg) of standard air that is in a room 10 ft by 10 ft by 8 ft, and then compute this mass in lbm and kg to see how close your estimate was. Solution Given: Dimensions of a room. Find: Mass of air in lbm and kg. The data for standard air are: R air 53.33 ft lbf lbmr p 14.7psi T ( 59 + 460) R 519R Then ρ p R air T ρ 14.7 lbf in 2 1 53.33 lbmr ftlbf 1 519R 12in 1ft 2 ρ 0.0765 lbm ft 3 or ρ 1.23 kg m 3 The volume of the room is V 10ft 10ft 8ft V 800ft 3 The mass of air is then m ρv m 0.0765 lbm ft 3 800ft 3 m 61.2 lbm m 27.8 kg

Problem 1.7 Given: Data on nitrogen tank Find: Mass of nitrogen Solution The given or available data is: D 6in L 4.25ft p 204atm T ( 59 + 460) R T 519R R N2 55.16 ft lbf lbr (Table A.6) The governing equation is the ideal gas equation p ρr N2 T and ρ M V where V is the tank volume V π 4 D2 L V π 4 2 6 V 0.834ft 3 12 ft 4.25ft Hence M Vρ pv R N2 T lbf M 204 14.7 in 2 144in 2 ft 2 0.834ft 3 1 55.16 lbr ftlbf 1 1 32.2 519 R lbft s 2 lbf M 12.6 lb M 0.391 slug

Problem 1.16 From Appendix A, the viscosity µ (N. s/m 2 ) of water at temperature T (K) can be computed from µ A10 B/(T - C), where A 2.414 X 10-5 N.s/m 2, B 247.8 K, and C 140 K. Determine the viscosity of water at 20 C, and estimate its uncertainty if the uncertainty in temperature measurement is +/- 0.25 C. Solution Given: Data on water. Find: Viscosity and uncertainty in viscosity. The data provided are: A 2.41410 5 Ns m 2 B 247.8K C 140K T 293K The uncertainty in temperature is u T 0.25K 293K u T 0.085% The formula for viscosity is B ( T C) µ ( T) A10 Evaluating µ 247.8K µ ( T) 2.41410 5 Ns ( 293K 140K) m 2 10 µ ( T) 1.005 10 3 Ns m 2 For the uncertainty B d dt µ ( T) ( T C) B A10 ( T C) 2 ln( 10)

so u µ ( T) T d µ ( T) T µ ( T) u B T ln( 10) T d ( T C) 2 u T Using the given data 247.8K u µ ( T) ln( 10) 293K ( 293K 140K) 2 0.085% u µ ( T) 0.61%

Problem 1.20 The height of a building may be estimated by measuring the horizontal distance to a point on t ground and the angle from this point to the top of the building. Assuming these measurements L 100 +/- 0.5 ft and θ 30 +/- 0.2 degrees, estimate the height H of the building and the uncertainty in the estimate. For the same building height and measurement uncertainties, use Excel s Solver to determine the angle (and the corresponding distance from the building) at which measurements should be made to minimize the uncertainty in estimated height. Evaluat and plot the optimum measurement angle as a function of building height for 50 < H < 1000 f Solution Given: Data on length and angle measurements. Find: The data provided are: L 100ft δl 0.5ft θ 30deg δθ 0.2deg The uncertainty in L is u L δl L u L 0.5% The uncertainty in θ is u θ δθ θ u θ 0.667% The height H is given by H Ltan( θ) H 57.7 ft For the uncertainty u H L H L Hu L 2 + θ H θ Hu θ 2

and L H tan( θ) θ H ( ( ) 2 ) L 1 + tan θ ( ) L so u H H tan θ u L 2 + ( ) Lθ H 1 + tan( θ)2 2 u θ Using the given data 100 u H 57.5 tan π 6 0.5 100 2 100 π 6 + 57.5 1 + tan π 6 2 0.667 100 2 u H 0.95% δh u H H δh 0.55 ft H 57.5 + 0.55ft The angle θ at which the uncertainty in H is minimized is obtained from the corresponding Exce workbook (which also shows the plot of u H vs θ) θ optimum 31.4deg

Problem 1.20 (In Excel) The height of a building may be estimated by measuring the horizontal distance to a point on the ground and the angle from this point to the top of the building. Assuming these measurements are L 100 +/- 0.5 ft and θ 30 +/- 0.2 degrees, estimate the height H of the building and the uncertainty in the estimate. For the same building height and measurement uncertainties, use Excel s Solver to determine the angle (and the corresponding distance from the building) at which measurements should be made to minimize the uncertainty in estimated height. Evaluate and plot the optimum measurement angle as a function of building height for 50 < H < 1000 ft. Given: Data on length and angle measurements. Find: Height of building; uncertainty; angle to minimize uncertainty Given data: H 57.7 ft δl 0.5 ft δθ 0.2 deg For this building height, we are to vary θ (and therefore L ) to minimize the uncertainty u H. ( ( ) 2 ) 2 The uncertainty is L u H H tan ( θ ) Lθ u L + H 1 + tan θ 2 u θ Expressing u H, u L, u θ and L as functions of θ, (remember that δl and δθ are constant, so as L and θ vary the uncertainties will too!) and simplifying Plotting u H vs θ ( ) tan( θ) δl 2 H u H θ ( ( ) 2 ) 1 + tan θ + tan( θ) 2 δθ θ (deg) u H 5 4.02% 10 2.05% 15 1.42% 20 1.13% 25 1.00% 30 0.949% 35 0.959% 40 1.02% 45 1.11% 50 1.25% 55 1.44% 60 1.70% 65 2.07% 70 2.62% 75 3.52% 80 5.32% 85 10.69% Optimizing using Solver u H 12% 10% 8% 6% 4% 2% 0% Uncertainty in Height (H 57.7 ft) vs θ 0 20 40 60 80 100 θ ( o )

θ (deg) u H 31.4 0.95% To find the optimum θ as a function of building height H we need a more complex Solver H (ft) θ (deg) u H 50 29.9 0.99% 75 34.3 0.88% 100 37.1 0.82% 125 39.0 0.78% 175 41.3 0.75% 200 42.0 0.74% 250 43.0 0.72% 300 43.5 0.72% 400 44.1 0.71% 500 44.4 0.71% 600 44.6 0.70% 700 44.7 0.70% 800 44.8 0.70% 900 44.8 0.70% 1000 44.9 0.70% θ (deg) 50 45 40 35 30 25 20 15 10 5 0 Optimum Angle vs Building Height 0 200 400 600 800 1000 H (ft) Use Solver to vary ALL θ's to minimize the total u H! Total u H 's: 11.32%

Problem 1.24 For a small particle of aluminum (spherical, with diameter d 0.025 mm) falling in standard air at speed V, the drag is given by F D 3πµVd, where µ is the air viscosity. Find the maximum speed starting from rest, and the time it takes to reach 95% of this speed. Plot the speed as a function of time. Solution Given: Data on sphere and formula for drag. Find: Maximum speed, time to reach 95% of this speed, and plot speed as a function of time. The data provided, or available in the Appendices, are: ρ air 1.17 kg m 3 µ 1.8 10 5 Ns m 2 ρ w 999 kg m 3 SG Al 2.64 d 0.025mm Then the density of the sphere is ρ Al SG Al ρ w ρ Al 2637 kg m 3 The sphere mass is πd 3 M ρ Al 6 2637 kg m 3 π ( 0.000025m) 3 6 M 2.16 10 11 kg Newton's 2nd law for the steady state motion becomes Mg 3π Vd so V max Mg 3 πµ d 1 3 π 2.16 10 11 kg m s 2 9.81 s 2 m 2 1.8 10 5 Ns 1 0.000025m

V max 0.0499 m s Newton's 2nd law for the general motion is M dv dt Mg 3 πµ Vd so g dv 3 πµ d V m dt Integrating and using limits Vt () Mg 3 πµ d 3 πµ d t M 1 e Using the given data 0.06 V (m/s) 0.04 0.02 0 0.005 0.01 0.015 0.02 t (s) The time to reach 95% of maximum speed is obtained from Mg 3 πµ d 3 πµ d t M 1 e 0.95V max so t M 0.95V max 3 πµ d ln 1 Substituting values t 0.0152s 3 πµ d Mg

Problem 1.24 (In Excel) For a small particle of aluminum (spherical, with diameter d 0.025 mm) falling in standard air at speed V, the drag is given by F D 3πµVd, where µ is the air viscosity. Find the maximum speed starting from rest, and the time it takes to reach 95% of this speed. Plot the speed as a function of time. Solution Given: Find: Data and formula for drag. Maximum speed, time to reach 95% of final speed, and plot. The data given or availabke from the Appendices is µ 1.80E-05 Ns/m 2 ρ 1.17 kg/m 3 SG Al 2.64 ρ w 999 kg/m 3 d 0.025 mm Data can be computed from the above using the following equations ρ Al SG Al ρ w Speed V vs Time t π d 3 M ρ Al 6 Mg V max 3 π µ d 3 πµ d Mg t M Vt () 1 e 3 π µ d t (s) V (m/s) ρ Al 2637 kg/m 3 0.000 0.0000 0.00 0.002 0.0162 M 2.16E-11 kg 0.004 0.0272 0.006 0.0346 Vmax 0.0499 m/s 0.008 0.0396 0.010 0.0429 0.012 0.0452 For the time at which V (t ) 0.95V max, use Goal Seek : 0.014 0.0467 0.016 0.0478 0.018 0.0485 t (s) V (m/s) 0.95V max Error (%) 0.020 0.0489 0.0152 0.0474 0.0474 0.04% 0.022 0.0492 0.024 0.0495 0.026 0.0496 V (m/s) 0.06 0.05 0.04 0.03 0.02 0.01 0.000 0.005 0.010 0.015 0.020 0.025 0.030 t (s)

Problem 1.25 For small spherical water droplets, diameter d, falling in standard air at speed V, the drag is given by F D 3πµVd, where µ is the air viscosity. Determine the diameter d of droplets that take 1 second to fall from rest a distance of 1 m. (Use Excel s Goal Seek.) Solution Given: Data on sphere and formula for drag. Find: Diameter of water droplets that take 1 second to fall 1 m. The data provided, or available in the Appendices, are: µ 1.8 10 5 Ns m 2 ρ w 999 kg m 3 Newton's 2nd law for the sphere (mass M) is M dv dt Mg 3 πµ Vd so g dv 3 πµ d V m dt Integrating and using limits Vt () Mg 3 πµ d 3 πµ d t M 1 e Integrating again xt () Mg 3 πµ d t + M 3 πµ d 3 πµ d t M e 1

πd 3 Replacing M with an expression involving diameter d M ρ w 6 xt () ρ w d 2 g 18 µ t + ρ w d 2 18 µ 18µ ρ w d 2 t e 1 This equation must be solved for d so that x( 1s ) 1m. The answer can be obtained from manual iteration, or by using Excel's Goal Seek. d 0.193mm 1 x (m) 0.5 0 0.2 0.4 0.6 0.8 1 t (s)

Problem 1.25 (In Excel) For small spherical water droplets, diameter d, falling in standard air at speed V, the drag is given by F D 3πµVd, where µ is the air viscosity. Determine the diameter d of droplets that take 1 second to fall from rest a distance of 1 m. (Use Excel s Goal Seek.) speed. Plot the speed as a function of time. Solution Given: Data and formula for drag. Find: Diameter of droplets that take 1 s to fall 1 m. The data given or availabke from the Appendices is µ 1.80E-05 Ns/m 2 ρ w 999 kg/m 3 Make a guess at the correct diameter (and use Goal Seek later): (The diameter guess leads to a mass.) d 0.193 mm M 3.78E-09 kg Data can be computed from the above using the following equations: π d 3 M ρ w 6 xt () Mg t + 3 π µ d M e 3 π µ d 3 πµ d t M 1 Use Goal Seek to vary d to make x (1s) 1 m: t (s) x (m) t (s) x (m) 1.000 1.000 0.000 0.000 0.050 0.011 0.100 0.037 Distance x vs Time t 0.150 0.075 0.200 0.119 1.20 0.250 0.167 0.300 0.218 1.00 0.350 0.272 0.80 0.400 0.326 0.450 0.381 0.60 0.500 0.437 0.550 0.492 0.40 0.600 0.549 0.650 0.605 0.20 0.700 0.661 0.750 0.718 0.00 0.000 0.200 0.400 0.600 0.800 1.000 1.200 0.800 0.774 t (s) 0.850 0.831 0.900 0.887 0.950 0.943 1.000 1.000 x (m)

Problem 1.30 Derive the following conversion factors: (a) Convert a pressure of 1 psi to kpa. (b) Convert a volume of 1 liter to gallons. (c) Convert a viscosity of 1 lbf.s/ft 2 to N.s/m 2. Solution Using data from tables (e.g. Table G.2) (a) 1psi 6895Pa 1kPa 1psi 6.89kPa 1psi 1000Pa (b) 1liter 1quart 1gal 1liter 0.264gal 0.946liter 4quart (c) 1 lbf s ft 2 2 1 1 lbf s 4.448N 12 ft ft 2 47.9 Ns 1lbf 0.0254m m 2

Problem 1.31 Derive the following conversion factors: (a) Convert a viscosity of 1 m 2 /s to ft 2 /s. (b) Convert a power of 100 W to horsepower. (c) Convert a specific energy of 1 kj/kg to Btu/lbm. Solution Using data from tables (e.g. Table G.2) (a) 1 m2 s 2 1 1 m2 12 ft 10.76 ft2 s 0.0254m s (b) 100W 1hp 100W 0.134hp 746W (c) 1 kj kg 1 kj 1000J 1Btu 0.454kg 0.43 Btu kg 1kJ 1055J 1lbm lbm

Problem 1.33 Derive the following conversion factors: (a) Convert a volume flow rate in in. 3 /min to mm 3 /s. (b) Convert a volume flow rate in cubic meters per second to gpm (gallons per minute). (c) Convert a volume flow rate in liters per minute to gpm (gallons per minute). (d) Convert a volume flow rate of air in standard cubic feet per minute (SCFM) to cubic meters per hour. A standard cubic foot of gas occupies one cubic foot at standard temperature and pressure (T 15 C and p 101.3 kpa absolute). Solution Using data from tables (e.g. Table G.2) (a) 1 in3 min 1 in3 3 0.0254m 1000mm 1min 273 mm3 min 1in 1m 60s s (b) 1 m3 s 1 m3 1quart 1gal 60s s 0.000946m 3 15850gpm 4quart 1min (c) 1 liter min 1 liter 1quart 1gal 60s 0.264 gal min 0.946liter 4quart 1min min (d) 1SCFM 1 ft3 3 0.0254m 60min min 1 1.70 m3 12 ft hr hr

Problem 1.35 Sometimes engineering equations are used in which units are present in an inconsistent manner. For example, a parameter that is often used in describing pump performance is the specific speed, NScu, given by 1 2 N( rpm) Q( gpm) N Scu 3 4 Hft ( ) What are the units of specific speed? A particular pump has a specific speed of 2000. What will be the specific speed in SI units (angular velocity in rad/s)? Solution Using data from tables (e.g. Table G.2) N Scu 1 2 rpmgpm 2000 2000 3 4 ft 1 2 rpmgpm 3 4 ft 2πrad 1rev 1min.. 60s 4quart 1gal 0.000946m 3 1quart 1min 60s 3 1 4 1 2 12 ft rad m 3 s s 4.06 0.0254m 3 4 m 1 2

Problem 1.36 A particular pump has an engineering equation form of the performance characteristic equatio given by H (ft) 1.5-4.5 x 10-5 [Q (gpm)] 2, relating the head H and flow rate Q. What are the units of the coefficients 1.5 and 4.5 x 10-5? Derive an SI version of this equation. Solution Dimensions of "1.5" are ft. Dimensions of "4.5 x 10-5 " are ft/gpm 2. Using data from tables (e.g. Table G.2), the SI versions of these coefficients can be obtained 1.5ft 0.0254m 1.5ft 0.457m 1 12 ft 4.5 10 5 ft gpm 2 4.510 5 ft gpm 2 0.0254m 1 12 ft 1gal 1quart 60s 4quart 0.000946m 3 1min 2 4.510 5 ft gpm 2 3450 m m 3 s 2 The equation is 2 Hm ( ) 0.457 3450 Q m3 s