Elements of Gas Dynamics /

The increasing importance of concepts from compressible fluid flow theory for aeronautical applications makes the republication of this first-rate text particularly timely. Intended mainly for aeronautics students, the text will also be helpful to practicing engineers and scientists who work on prob...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Liepmann, H. W. (Hans Wolfgang), 1914-2009 (Autor)
Formato: Electrónico eBook
Idioma:Inglés
Publicado: New York : Dover Publications, 2013.
Temas:
Gas dynamics.
Aerodynamics.
Dynamique des gaz.
Aérodynamique.
aerodynamics.
SCIENCE > Mechanics > General.
Aerodynamics
Gas dynamics
Acceso en línea:Texto completo
Tabla de Contenidos:
  • Cover; Title Page; Copyright Page; Editors' Preface; Authors' Preface; Contents; Chapter 1. Concepts from Thermodynamics; 1.1
  • Introduction; 1.2
  • Thermodynamic Systems; 1.3
  • Variables of State; 1.4
  • The First Principal Law; 1.5
  • Irreversible and Reversible Processes; 1.6
  • Perfect Gases; 1.7
  • The First Law Applied to Reversible Processes. Specific Heats; 1.8
  • The First Law Applied to Irreversible Processes; 1.9
  • The Concept of Entropy. The Second Law; 1.10
  • The Canonical Equation of State. Free Energy and Free Enthalpy; 1.11
  • Reciprocity Relations
  • 1.12
  • Entropy and Transport Processes1.13*
  • Equilibrium Conditions; 1.14*
  • Mixtures of Perfect Gases; 1.15*
  • The Law of Mass Action; 1.16*
  • Dissociation; 1.17*
  • Condensation; 1.18
  • Real Gases in Gasdynamics; Chapter 2. One-Dimensional Gasdynamics; 2.1
  • Introduction; 2.2
  • The Continuity Equation; 2.3
  • The Energy Equation; 2.4
  • Reservoir Conditions; 2.5
  • Euler's Equation; 2.6
  • The Momentum Equation; 2.7
  • Isentropic Conditions; 2.8
  • Speed of Sound; Mach Number; 2.9
  • The Area-Velocity Relation; 2.10
  • Results from the Energy Equation; 2.11
  • Bernoulli Equation; Dynamic Pressure
  • 2.12
  • Flow at Constant Area2.13
  • The Normal Shock Relations for a Perfect Gas; Chapter 3. One-Dimensional Wave Motion; 3.1
  • Introduction; 3.2
  • The Propagating Shock Wave; 3.3
  • One-Dimensional Isentropic Equations; 3.4
  • The Acoustic Equations; 3.5
  • Propagation of Acoustic Waves; 3.6
  • The Speed of Sound; 3.7
  • Pressure and Particle Velocity in a Sound Wave; 3.8
  • "Linearized" Shock Tube; 3.9
  • Isentropic Waves of Finite Amplitude; 3.10
  • Propagation of Finite Waves; 3.11
  • Centered Expansion Wave; 3.12
  • The Shock Tube; Chapter 4. Waves in Supersonic Flow; 4.1
  • Introduction
  • 4.20*
  • The Hodograph Plane4.21
  • Cone in Supersonic Flow; Chapter 5. Flow in Ducts and Wind Tunnels; 5.1
  • Introduction; 5.2
  • Flow in Channel of Varying Area; 5.3
  • Area Relations; 5.4
  • Nozzle Flow; 5.5
  • Normal Shock Recovery; 5.6
  • Effects of Second Throat; 5.7
  • Actual Performance of Wind Tunnel Diffusers; 5.8
  • Wind Tunnel Pressure Ratio; 5.9
  • Supersonic Wind Tunnels; 5.10
  • Wind Tunnel Characteristics; 5.11
  • Compressor Matching; 5.12
  • Other Wind Tunnels and Testing Methods; Chapter 6. Methods of Measurement; 6.1
  • Introduction; 6.2
  • Static Pressure; 6.3
  • Total Pressure
  • 6.4
  • Mach Number from Pressure Measurements

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