EGN 3353C Fluid Mechanics

Similar documents
5. Dimensional Analysis. 5.1 Dimensions and units

[95/95] APPROACH FOR DESIGN LIMITS ANALYSIS IN VVER. Shishkov L., Tsyganov S. Russian Research Centre Kurchatov Institute Russian Federation, Moscow

AN EXPLICIT METHOD FOR NUMERICAL SIMULATION OF WAVE EQUATIONS

VACUUM chambers have wide applications for a variety of

Frequency Domain Analysis of Rattle in Gear Pairs and Clutches. Abstract. 1. Introduction

Numerical Method for Obtaining a Predictive Estimator for the Geometric Distribution

Phase field modelling of microstructural evolution using the Cahn-Hilliard equation: A report to accompany CH-muSE

CAUCHY PROBLEM FOR TECHNOLOGICAL CUMULATIVE CHARGE DESIGN. Christo Christov, Svetozar Botev

Proceedings of Meetings on Acoustics

The Realm of Hydrogeology

INTERIOR BALLISTIC PRINCIPLE OF HIGH/LOW PRESSURE CHAMBERS IN AUTOMATIC GRENADE LAUNCHERS

The CIA (consistency in aggregation) approach A new economic approach to elementary indices

SUPPORTING INFORMATION FOR. Mass Spectrometrically-Detected Statistical Aspects of Ligand Populations in Mixed Monolayer Au 25 L 18 Nanoparticles

Isothermal Elastohydrodynamic Lubrication. E. Feyzullahoglu

Wind Loading for the Design of the Solar Tower

1. (2.5.1) So, the number of moles, n, contained in a sample of any substance is equal N n, (2.5.2)

Why do Golf Balls have Dimples on Their Surfaces?

Outline. Review for Final Exam. But, First a Word About Units. The Final. Transitions Between Phases. Density and Related Summary

MATHEMATICAL MODELS AND OPTICAL INVESTIGATION OF TWO PHASE FLOWS IN WIND TUNNELS

The Number of Information Bits Related to the Minimum Quantum and Gravitational Masses in a Vacuum Dominated Universe

CHAPTER 2 THERMODYNAMICS

3 Thermodynamics and Statistical mechanics

Minimizing Machinery Vibration Transmission in a Lightweight Building using Topology Optimization

16.333: Lecture # 7. Approximate Longitudinal Dynamics Models

An Investigation into the Effects of Roll Gyradius on Experimental Testing and Numerical Simulation: Troubleshooting Emergent Issues

Discover the answer to this question in this chapter.

Binomial and Poisson Probability Distributions

Fundamentals of Astrodynamics and Applications 3 rd Ed

Computationally Efficient Control System Based on Digital Dynamic Pulse Frequency Modulation for Microprocessor Implementation

3.8. External Source in Quantum-Statistical Path Integral

Control and Stability of the Time-delay Linear Systems

Efforts Towards a Validated Time-Domain Model of an Oscillating Water Column with Control Components

Quadratic Reciprocity. As in the previous notes, we consider the Legendre Symbol, defined by

The Open Civil Engineering Journal

Dimensions and Units

Lecture 13 Eigenvalue Problems

Broadband Synthetic Aperture Matched Field Geoacoustic Inversion

Numerical Model of the Human Head under Side Impact

Exploiting Matrix Symmetries and Physical Symmetries in Matrix Product States and Tensor Trains

Donald Fussell. October 28, Computer Science Department The University of Texas at Austin. Point Masses and Force Fields.

I. Understand get a conceptual grasp of the problem

Electromagnetics I Exam No. 3 December 1, 2003 Solution

Design of Robust Reference Input Tracker via Delayed Feedback Control Method

Ufuk Demirci* and Feza Kerestecioglu**

arxiv: v1 [physics.soc-ph] 5 Jun 2011

EGN 3353C Fluid Mechanics

Kinematics and dynamics, a computational approach

On spinors and their transformation

USEFUL HINTS FOR SOLVING PHYSICS OLYMPIAD PROBLEMS. By: Ian Blokland, Augustana Campus, University of Alberta

STRAIN ENERGY DENSITY AS THE LINK BETWEEN GLOBAL AND LOCAL APPROACH TO FRACTURE

Experimental Determination of Flow and Heat Transfer Correlations for Passive Regenerators

On the characterization of non-linear diffusion equations. An application in soil mechanics

A Simplified Analytical Approach for Efficiency Evaluation of the Weaving Machines with Automatic Filling Repair

Included in this hand-out are five examples of problems requiring the solution of a system of linear algebraic equations.

Model for Determination of Protective Shielding Thickness for Diagnostic Radiology Rooms. P. R. Costa 1, L. V. E. Caldas 2

The Semantics of Data Flow Diagrams. P.D. Bruza. Th.P. van der Weide. Dept. of Information Systems, University of Nijmegen

Easy Evaluation Method of Self-Compactability of Self-Compacting Concrete

Thermal-hydraulic Modeling and Simulation of Piston Pump

arxiv: v4 [math.st] 9 Aug 2017

arxiv: v2 [math.st] 13 Feb 2018

4 A Survey of Congruent Results 12

The Wilson Model of Cortical Neurons Richard B. Wells

SIMILARITY CONDITIONS FOR LATERAL LOAD TEST ON MODEL PILE FOUNDATION WITH LARGE DEFORMATION IN 1G GRAVITATIONAL FIELD

DIRECT NUMERICAL SIMULATION OF HEAT TRANSPORT IN DISPERSED GAS-LIQUID TWO-PHASE FLOW USING A FRONT TRACKING APPROACH

New Set of Rotationally Legendre Moment Invariants

New Methodology for Estimating Unconventional Production and Long Term Performance

BALLISTIC PENDULUM. EXPERIMENT: Measuring the Projectile Speed Consider a steel ball of mass

Unsteady MHD free Convective flow in a Rotating System with Soret Effect on n th order chemical reaction S.Anuradha 1 K.Sasikala 2

doi: / ( / )

Anomalous heat capacity for nematic MBBA near clearing point

MODELING AND CONTROL OF A MICROGRIPPER BASED ON ELECTROMAGNETIC ACTUATION

Suppress Parameter Cross-talk for Elastic Full-waveform Inversion: Parameterization and Acquisition Geometry

Physically Based Modeling CS Notes Spring 1997 Particle Collision and Contact

arxiv: v2 [hep-ph] 2 Mar 2018

RESOLVENT ESTIMATES FOR ELLIPTIC SYSTEMS IN FUNCTION SPACES OF HIGHER REGULARITY

CALCULATION of CORONA INCEPTION VOLTAGES in N 2 +SF 6 MIXTURES via GENETIC ALGORITHM

Parallelizing Spectrally Regularized Kernel Algorithms

CDS 101: Lecture 5-1 Reachability and State Space Feedback. Review from Last Week

EE 434 Lecture 16. Small signal model Small signal applications in amplifier analysis and design

Ph 20.3 Numerical Solution of Ordinary Differential Equations

Dual porosity DRM formulation for flow and transport through fractured porous media

Handout 6 Solutions to Problems from Homework 2

Input-Output (I/O) Stability. -Stability of a System

In this lecture... Axial flow turbine Impulse and reaction turbine stages Work and stage dynamics Turbine blade cascade

FRESNEL FORMULAE FOR SCATTERING OPERATORS

NONNEGATIVE matrix factorization finds its application

DISTRIBUTION OF THE HYDRAULIC PARAMETERS AT RIVER BENDS

Massachusetts Institute of Technology Quantum Mechanics I (8.04) Spring 2005 Solutions to Problem Set 4

Current, Resistance Electric current and current density

Nonlinear Active Noise Control Using NARX Model Structure Selection

the static friction is replaced by kinetic friction. There is a net force F net = F push f k in the direction of F push.

Design of Linear-Phase Two-Channel FIR Filter Banks with Rational Sampling Factors

Tactics Box 2.1 Interpreting Position-versus-Time Graphs

Notes on Optical Pumping Procedure & Theory

Problem Set 2. Chapter 1 Numerical:

Modi ed Local Whittle Estimator for Long Memory Processes in the Presence of Low Frequency (and Other) Contaminations

Analytical Analysis and Feedback Linearization Tracking Control of the General Takagi-Sugeno Fuzzy Dynamic Systems

Inverse magnetoelectric effect in disk samples of ferrite piezoelectric composites

Modeling soft Scandinavian clay behavior using the asymptotic state

On the Effect of the Lambda Parameter on Performance and Stability Indexes in DMC Control

Transcription:

Lecture 4 When nondiensionalizing an equation, nondiensional araeters often aear. Exale Consider an object falling due to gravity in a vacuu d z ays: (1) the conventional diensional aroach, and () diensionless aroach. Integrating tice and alying the initial elevation z and velocity 1 z z t gt = + diensional anser dt = g. We ill solve for the elevation z to If e ant to deterine z( t ), e need to secify z,, and g (3 araeters). If one of these changes, e have to reeat the calculation! Instead e can nondiensionalize the above equation by z to give No define soe ne diensionless variables: The last ter becoes z t 1 gt = 1+ z z z * ( ) z z t =, t = z z * * t 1 g t z 1 * = = t z 1 g. The boxed ter is a diensionless z araeter. It is related to the ell-knon oude nuber = in Fluid Dynaics. MAE Det.

So the solution can be ritten in diensional or nondiensional for as follos: 1 z z t gt = + or z 1 t = 1+ t * * Ignoring tie, nd equation is only a function of 1 araeter * =, hile the first is a function of 3! Key Point: If you had to coute a table of solutions z( t ), you ould have to ick several different values of z,, and g and then calculate z( t ). If you choose 5 different values for each, that s 5 5 5 = 15 * * lots! On the other hand, you only have to lot z ( t ) for several different values of values of ). To calculate z( t ), just read convert t to t * and read = (5 different * z fro the aroriate lot (erhas using interolation) and then convert * z to z. o In suary, there are key advantages of nondiensionalization: 1. it increases our insight about the relationshis beteen key araeters = shos that doubling is equivalent to reducing g or z by a factor of four. it reduces the nuber of araeters in the roble 15 lots vs. 5! MAE Det.

Trajectories of a steel ball falling in a vacuu. The results are nondiensionalized. This lot ould even be valid for variable g. Trajectories of a steel ball falling in a vacuu: (a) fixed at 4 /s, and (b) z fixed at 1 (Exale 7 3). Here, g is fixed. MAE Det.

DIMENSIONAL ANALYSIS AND SIMILARITY o Engineering often requires exerients (nuerical siulations or hysical) on geoetrically scaled odels rather than full-scale rototyes o To do this roerly requires a tool called diensional analysis o Three riary uroses 1. To generate nondiensional araeters that hel in the design of exerients (hysical and/or nuerical) and in the reorting of exeriental results. To obtain scaling las so that rototye erforance can be redicted fro odel erforance 3. To (soeties) redict trends in the relationshi beteen araeters Underlying concet siilarity o Three necessary conditions ust be satisfied beteen a odel and a rototye 1. geoetric siilarity (odel and rototye have exactly the sae shae and differ only by a scale factor). kineatic siilarity (V at any oint differs only by a constant scale factor beteen odel and rototye) geoetric siilarity is a rerequisite for kineatic siilarity ilies that all kineatic features (strealines, vorticity, etc.) ill be identical in odel and rototye MAE Det.

3. dynaic siilarity (all F and M scale by a constant factor beteen odel and rototye) kineatic siilarity is a rerequisite for dynaic siilarity o In a general flo field, colete siilarity beteen a odel and rototye is achieved only hen there is dynaic siilarity (since dynaic siilarity ilies geoetric and kineatic siilarity) Diensionless Paraeters called Π araeters or grous o Usually ritten in folloing for Π = f Π, Π, Π,..., Π k 1 3 4 deendent indeendent araeters araeter o total of k Π grous e ill sho a rocedure to deterine these Π grous o Don t kno functional for of f need exerients to deterine this in general o if dynaic siilarity is achieved, all Π s ill be equal beteen odel and rototye MAE Det.

Exale Aerodynaic drag on a car. Wind tunnel test at sae conditions (sae fluid @ sae teerature). What is the velocity and force scale factors for dynaic siilarity? We ill see that there are only Π grous for incoressible flo over a car. FD Π 1 =, Π = V L drag coefficient VL μ Reynolds nuber Model ust be an exact relica (usually saller) of the rototye. Hence, Π =Π and Π =Π. 1 1 For 1/5 th scale odel for air ind tunnel (sae fluid @ sae teerature): VL μ VL L μ = or V = V = 5V. μ L μ = 1 = 5 = 1 If V = 55 h, V = h! Might be too high and ight FD FD violate incoressible assution. Also, = V L V L or L V FD = F D = F D. L V = 1 = 5 = 1/5 MAE Det.