Internal pressures Wind loading and structural response Lecture 16 Dr. J.D. Holmes.

Slides:



Advertisements
Similar presentations
Integration Relation for Control Volume
Advertisements

Experiment #5 Momentum Deficit Behind a Cylinder
Aero-Hydrodynamic Characteristics
Continuity Equation. Continuity Equation Continuity Equation Net outflow in x direction.
Ch 3.8: Mechanical & Electrical Vibrations
Boundary Layer Flow Describes the transport phenomena near the surface for the case of fluid flowing past a solid object.
..perhaps the hardest place to use Bernoulli’s equation (so don’t)
Who Wants to Be a CFD Expert? In the ME 566 course title, CFD for Engineering Design, what does the acronym CFD stand for? A.Car Free Day B.Cash Flow Diagram.
The Art of Comparing Force Strengths… P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Diagnosis of NS Equations.
Computer Aided Thermal Fluid Analysis Lecture 10
Wind loading and structural response Lecture 19 Dr. J.D. Holmes
Basic bluff-body aerodynamics I
Atmospheric boundary layers and turbulence II Wind loading and structural response Lecture 7 Dr. J.D. Holmes.
1 MECH 221 FLUID MECHANICS (Fall 06/07) Tutorial 7.
Fluid Mechanics –For Civil Engineers is all about SMU Storing– Moving– Using ( Incompressible fluids - water) To design and manage these systems we need.
Mark Claywell & Donald Horkheimer University of Minnesota
Sensible heat flux Latent heat flux Radiation Ground heat flux Surface Energy Budget The exchanges of heat, moisture and momentum between the air and the.
MECH 221 FLUID MECHANICS (Fall 06/07) Chapter 9: FLOWS IN PIPE
Physics of Sound Wave equation: Part. diff. equation relating pressure and velocity as a function of time and space Nonlinear contributions are not considered.
California State University, Chico
Intro to PLUS by Leta Moser and Kristen Cetin PLUS accreditation Peer-Led Undergraduate Studying (PLUS) –assists students enrolled by offering class- specific,
S1-1 SECTION 1 REVIEW OF FUNDAMENTALS. S1-2 n This section will introduce the basics of Dynamic Analysis by considering a Single Degree of Freedom (SDOF)
FUNDAMENTAL EQUATIONS, CONCEPTS AND IMPLEMENTATION
Wind loading and structural response Lecture 18 Dr. J.D. Holmes
Stirling-type pulse-tube refrigerator for 4 K
Basic structural dynamics II
Towers, chimneys and masts
In Engineering --- Designing a Pneumatic Pump Introduction System characterization Model development –Models 1, 2, 3, 4, 5 & 6 Model analysis –Time domain.
Aerodynamics Linear Motion (Moving Air ).
Basic bluff-body aerodynamics II
2-D Modeling of a Walking Human-clothing System. Motivation When people are active, the air spacing between the fabric layer of a porous clothing system.
Feb 18, /34 Mechanical Engineering at Virginia Tech What to bring and what to study One 8.5 X 11 formula sheet, one side only, no examples. Save.
CP502 Advanced Fluid Mechanics
Momentum Equations in a Fluid (PD) Pressure difference (Co) Coriolis Force (Fr) Friction Total Force acting on a body = mass times its acceleration (W)
CP502 Advanced Fluid Mechanics Compressible Flow Lectures 1 & 2 Steady, quasi one-dimensional, isothermal, compressible flow of an ideal gas in a constant.
Historically the First Fluid Flow Solution …. P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Second Class of Simple Flows.
Dimensional Analysis A tool to help one to get maximum information from a minimum number of experiments facilitates a correlation of data with minimum.
Along-wind dynamic response
Student Chapter Meeting Thursday, Sept. 3 rd 7pm ECJ Interested in HVAC design, MEP, or building environmental systems? Come learn about all of the.
Chapter 15FLUIDS 15.1 Fluid and the World Around Us 1.A fluid is a substance that cannot support a shearing stress. 2.Both gases and liquids are fluids.
Aerodynamic Forces Lift and Drag.
PAT328, Section 3, March 2001MAR120, Lecture 4, March 2001S14-1MAR120, Section 14, December 2001 SECTION 14 STRUCTURAL DYNAMICS.
Measurements in Fluid Mechanics 058:180:001 (ME:5180:0001) Time & Location: 2:30P - 3:20P MWF 218 MLH Office Hours: 4:00P – 5:00P MWF 223B-5 HL Instructor:
Basic structural dynamics I Wind loading and structural response - Lecture 10 Dr. J.D. Holmes.
Dr. Jason Roney Mechanical and Aerospace Engineering
Convection in Flat Plate Boundary Layers P M V Subbarao Associate Professor Mechanical Engineering Department IIT Delhi A Universal Similarity Law ……
INTRODUCTION TO CONVECTION
DIMENSIONAL ANALYSIS SECTION 5.
Scales of Motion, Reynolds averaging September 22.
Effective static loading distributions Wind loading and structural response Lecture 13 Dr. J.D. Holmes.
Wind damage and mechanics of flying debris Wind loading and structural response Lecture 2 Dr. J.D. Holmes.
Monday April 26, PHYS , Spring 2004 Dr. Andrew Brandt PHYS 1443 – Section 501 Lecture #24 Monday, April 26, 2004 Dr. Andrew Brandt 1.Fluid.
Pipe flow analysis.
Flow of Compressible Fluids. Definition A compressible flow is a flow in which the fluid density ρ varies significantly within the flowfield. Therefore,
Viscosità Equazioni di Navier Stokes. Viscous stresses are surface forces per unit area. (Similar to pressure) (Viscous stresses)
Chapter 11 DIMENSIONAL ANALYSIS. 2 Fundamental theory preliminary expt. Dimensional analysis: ( 因次分析 ) Experiments Practical Problems analytical soln.
1 Dept. of Agricultural & Biological Engineering University of Illinois TSM 363 Fluid Power Systems TSM 363 Fluid Power Systems Bernoulli’s Law and Applications.
ABE 223 ABE Principles – Machine systems Bernoulli’s Law Tony Grift
Lecture Objectives: Discus HW 1 Finish with Solar Radiation Components
Lecture Objectives: Answer questions related to HW 1
Lecture Objectives: Answer questions related to HW 1
Chapter 6A: INFILTRATION BACKGROUND
ME321 Kinematics and Dynamics of Machines
ME321 Kinematics and Dynamics of Machines
FLUID MECHANICS REVIEW
Part VI:Viscous flows, Re<<1
Convective Heat Transfer
CHAPTER FIVE FANNO FLOW 5.1 Introduction
Asst. Prof. Dr. Hayder Mohammad Jaffal
Lecture 4 Dr. Dhafer A .Hamzah
Presentation transcript:

Internal pressures Wind loading and structural response Lecture 16 Dr. J.D. Holmes

Internal pressures Wind pressure on a wall cladding or roof is always : external wind pressure - internal pressure wind will affect internal pressure magnitude, except for fully sealed buildings Fully-sealed buildings : assume internal pressure is atmospheric pressure (p o ) Wind-induced internal pressures significant for dominant openings - e.g. produced by flying debris

Internal pressures Single opening on windward wall air flow into building  increase in density of air within the volume external pressure changes produced by wind - typically 1% of absolute air pressure internal pressure responds quickly to external flow and pressure changes Single Dominant Opening

Internal pressures Single opening on windward wall Dimensional analysis :  1 = A 3/2 /V o - where A is the area of the opening, and V o is the internal volume - where p o is atmospheric (static) pressure (related to Mach Number)  3 =  a  UA 1/2 /  - where  is the dynamic viscosity of air (Reynolds Number) (turbulence intensity)  5 = u /  A - where u is the length scale of turbulence

Internal pressures Single opening on windward wall Helmholtz resonator model : Air ‘slug’ moves in and out of building in response to external pressures Air ‘slug’ Mixing of moving air is ignored e

Internal pressures Single opening on windward wall Helmholtz resonator model : inertial term (mass times acceleration) for air slug damping - energy losses through opening stiffness - resistance of internal pressure to movement of slug A = area of opening, V o = internal volume  a = (external) air density, p o = (external) air pressure

Internal pressures Single opening on windward wall ‘Stiffness’ term : Assume adiabatic law for internal pressure and density Since  i   a, p i  p o Resisting force =  p i.A  = ratio of specific heats(1.4 for air)

Internal pressures Single opening on windward wall ‘Damping’ term : From steady flow through a sharp-edged orifice : k = discharge coefficient Theoretically k = Inertial term : Theoretically e =(circular opening)

Internal pressures Single opening on windward wall Converting to pressure coefficients : Second-order differential equation for C pi (t) Undamped natural frequency (Helmholtz frequency) : Increase internal volume V o : decrease resonant frequency, increase damping Increase opening area A : increase resonant frequency, decrease damping

Internal pressures Single opening on windward wall Helmholtz resonant frequency : Effect of building flexibility : K A = bulk modulus of air = pressure change for unit change in volume = (  a  p)/ , equal to  p o K B = bulk modulus for the building For low-rise buildings, K A / K B = 0.2 to 5 (for Texas Tech field building, K A / K B = 1.5)

Internal pressures Single opening on windward wall Helmholtz resonant frequency : (measured values for Texas Tech building) Resonant response is not high because of high damping

Internal pressures Single opening on windward wall Sudden windward opening (e.g. window failure) : Small opening area - high damping Large opening area - low damping - overshoot and oscillations V o = 600 m 3. A w = 1m 2. U = 30 m/s Time (secs ) Cp i V o = 600 m 3. A w = 9m 2. U = 30 m/s Time (secs) Cp i

Internal pressures Multiple openings on windward and leeward walls : Neglecting compressibility in this case (  a = 0) : Can be used for mean internal pressures or peak pressures using quasi-steady assumption. Need iterative solution when N is large. where (modulus allows for flow from interior to exterior) N is number of openings

Internal pressures Multiple openings on windward and leeward walls : Consider building with 5 openings : Q1Q1 Q2Q2 Q3Q3 Q4Q4 Q5Q5 p e,1 p e,2 p e,3 p e,4 p e,5 pipi inflows outflows

Internal pressures Single windward opening and single leeward opening : i.e. 2 openings : in terms of pressure coefficients, Equation 6.16 in book re-arranging,

Internal pressures Single windward opening and single leeward opening : i.e. comparison with experimental data : Used in codes and standards to predict peak pressures (quasi-steady principle) A W /A L  C pi Measurements Equation (6.16)

Internal pressures Multiple windward and leeward openings : Neglect inertial terms, characteristic response time : Characteristic frequency, n c = 1/(2  c ) A w = combined opening area on windward wall A L = combined opening area on leeward wall fluctuating internal pressures : numerical solutions required if inertial terms are included

Internal pressures Multiple windward and leeward openings : Effective standard deviation of velocity fluctuations filtered by building : High characteristic frequency - most turbulence fluctuations appear as internal pressures Low characteristic frequency - most turbulence fluctuations do not appear as internal pressures

Internal pressures Porous buildings : Treated in same way as multiple windward and leeward openings : A L = average wall porosity  total areas of leeward and side walls A w = average wall porosity  total windward wall area

End of Lecture 16 John Holmes