e52a6f0149 Next:. Previous:. degree) in 1946 in mechanical engineering from MIT. from The Metalogicon by John in 1159 Notice of Copyright For This Document: GNU Free Documentation License Potto Project License CONTRIBUTOR LIST How to contribute to this book Credits John Martones Grigory Toker Ralph Menikoff Your name here Typo corrections and other "minor" contributions About This Author Prologue For The POTTO Project Prologue For This Book Version 0.4.3 Sep. E.R.G.Eckert. Unfortunately for the field of Gas Dynamics, Shapiro moved to the field of biomedical engineering where he was able to pioneer new work. Dailymotion Info Pers Vacatures Blog Alle videos Zakelijk Adverteren op Dailymotion Monetizing Help Familie Filter AAN Help Center Contact Juridische voorwaarden Gebruiksvoorwaarden Privacybeleid Verboden video content Copyrightkennisgeving Kinder bescherming Cookiesbeleid Extra's Dailymotion Games Dailymotion Overal Dailymotion Stream Jukebox meer.
(It is M.I.T.'s equivalent of a Ph.D. Furthermore, Shapiro's knowledge of fluid mechanics enabled him to sew'' the missing parts of the Fanno line with Moody's diagram to create the most useful model in compressible flow. Door gebruik te maken van Dailymotion, geeft u toestemming voor onze cookies. 15, 2006 Version 0.4.2 Version 0.4 Version 0.3 How This Book Was Written About Gas Dynamics Calculator Version 0.5 Version 0.4.3 Version 0.4.1.7 Preface To Do List and Road Map Speed of Sound Stagnation effects Nozzle Normal Shock Isothermal Flow Fanno Flow Rayleigh Flow Evacuation and filling semi rigid Chambers Evacuating and filling chambers under external forces Oblique Shock Prandtl-Meyer Transient problem Introduction What is Compressible Flow ? Why Compressible Flow is Important? Historical Background Early Developments Speed of Sound The shock wave puzzle Choking Flow Nozzle Flow Nozzle flow Rayleigh Flow Fanno Flow Isothermal Flow External flow Filling and Evacuating Gaseous Chambers Biographies of Major Figures Galileo Galilei Ernest Mach (1838-1916) John William Strutt (Lord Rayleigh) William John Macquorn Rankine Gino Girolamo Fanno Ludwig Prandtl E.R.G.Eckert Ascher Shapiro Fundamentals of Basic Fluid Mechanics Introduction Fluid Properties Control Volume Reynold's Transport Theorem Speed of Sound Motivation Introduction Speed of sound in ideal and perfect gases Speed of Sound in Real Gas Speed of Sound in Almost Incompressible Liquid Speed of Sound in Solids Sound Speed in Two Phase Medium Isentropic Flow Stagnation State for Ideal Gas Model General Relationship Relationships for Small Mach Number Isentropic Converging-Diverging Flow in Cross Section The Properties in the Adiabatic Nozzle The pressure Mach number relationship Relationship Between the Mach Number and Cross Section Area Isentropic Flow Examples Mass Flow Rate (Number) Naughty Professor'' Problems in Isentropic Flow Flow with pressure losses Isentropic Tables Isentropic Isothermal Flow Nozzle General Relationship The Impulse Function Impulse in Isentropic Adiabatic Nozzle The Impulse Function in Isothermal Nozzle Isothermal Table The effects of Real Gases Normal Shock Solution of the Governing Equations Informal Model Formal Model The Maximum Conditions The Star Conditions Prandtl's Condition Operating Equations and Analysis The Limitations of the Shock Wave Small Perturbation Solution Shock Thickness Shock or Wave Drag The Moving Shocks Shock or Wave Drag Result from a Moving Shock Shock Result from a Sudden and Complete Stop Moving Shock into Stationary Medium (Suddenly Open Valve) General Velocities Issues Shock-Choke Phenomenon Partially Open Valve Partially Closed Valve Worked-out Examples for Shock Dynamics Shock Tube Shock with Real Gases Shock in Wet Steam Normal Shock in Ducts More Examples for Moving Shocks Tables of Normal Shocks, k=1.4 Ideal Gas Normal Shock in Variable Duct Areas Nozzle efficiency Diffuser Efficiency Nozzle Flow With External Forces Isentropic Nozzle (Q=0) Isothermal Nozzle (T=constant) Isothermal Flow The Control Volume Analysis/Governing equations Dimensionless Representation The Entrance Limitation of Supersonic Branch Comparison with Incompressible Flow Supersonic Branch Figures and Tables Isothermal Flow Examples Unchoked situations in Fanno Flow Fanno Flow Introduction Model Non-Dimensionalization of the Equations The Mechanics and Why the Flow is Choked? Why the flow is choked? The Trends The working equations Examples of Fanno Flow Supersonic Branch Maximum Length for the Supersonic Flow Working Conditions Variations of The Tube Length (4fL/D) Effects Fanno Flow Subsonic branch Fanno Flow Supersonic Branch The Pressure Ratio, P2/P1, effects Choking explanation for pressure variation/reduction Fanno Flow Short 4fL/D Long 4fL/D Entrance Mach number, M1, effects The Practical Questions and Examples of Subsonic branch Subsonic Fanno Flow for Given 4fL/D and Pressure Ratio Subsonic Fanno Flow for a Given Entrance Mach Number and Pressure Ratio The Approximation of the Fanno Flow by Isothermal Flow More Examples of Fanno Flow The Table for Fanno Flow Rayleigh Flow Introduction Governing Equation Rayleigh Flow Tables Examples For Rayleigh Flow Evacuating SemiRigid Chambers Governing Equations and Assumptions General Model and Non-dimensioned Isentropic Process Isothermal Process in The Chamber A Note on the Entrance Mach number Rigid Tank with Nozzle Adiabatic Isentropic Nozzle Attached Filling/Evacuating The Chamber Under Upchucked Condition Isothermal Nozzle Attached Rapid evacuating of a rigid tank With Fanno Flow Filling Process The Isothermal Process Simple Semi Rigid Chamber The Simple'' General Case Advance Topics Evacuating under External Volume Control General Model Rapid Process Examples Direct Connection Summary Oblique Shock Preface to Oblique Shock Introduction Introduction to Oblique Shock Introduction to Prandtl-Meyer Function Introduction to Zero Inclination Oblique Shock Solution of Mach Angle Upstream Mach number, M1, and deflection angle, δ The case of D >= 0 or 0 >= delta Upstream Mach Number, M1, and Shock Angle, θ Given Two Angles, δ and θ Flow in a Semi-2D Shape Small δ Weak Oblique shock'' Close and Far Views of the Oblique Shock Maximum Value of Oblique shock Detached Shock Issues Related to the Maximum Deflection Angle Oblique Shock Examples Application of Oblique Shock Optimization of Suction Section Design Retouch of Shock or Wave Drag Summary Appendix: Oblique Shock Stability Analysis Prandtl-Meyer Function Introduction Geometrical Explanation Alternative Approach to Governing Equations Comparison And Limitations between the Two Approaches The Maximum Turning Angle The Working Equations for the Prandtl-Meyer Function d'Alembert's Paradox Examples For Prandtl-Meyer Function Combination of the Oblique Shock and Isentropic Expansion Computer Program About the Program Usage Program listings Index About this document . MIT Professor Ascher Shapiro1.52, the Eckert equivalent for the compressible flow, was instrumental in using his two volume book The Dynamics of Thermodynamics of the Compressible Fluid Flow,'' to transform the gas dynamics field to a coherent text material for engineers. Inschrijven Uw selectie Categorien Alle categorien Kanaal suggesties . Next: Fundamentals of Basic Fluid Up: Biographies of Major Figures Previous: E.R.G.Eckert Index Created by:Genick Bar-Meir, Ph.D.. Go to Potto home. Index. He was assistant professor in 1943, three years before receiving his Sc.D.
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