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Detonation and Two-Phase Flow.

By: Contributor(s): Material type: TextTextSeries: Progress in Astronautics and AeronauticsPublisher: Reston : American Institute of Aeronautics and Astronautics, 1961Copyright date: ©1962Edition: 1st edDescription: 1 online resource (381 pages)Content type:
  • text
Media type:
  • computer
Carrier type:
  • online resource
ISBN:
  • 9781600862618
Subject(s): Genre/Form: Additional physical formats: Print version:: Detonation and Two-Phase FlowLOC classification:
  • QD516.S96 1962
Online resources:
Contents:
Cover -- Title -- Copyright -- Propellants and Combustion Committee -- Liquid Rockets Committee -- Preface -- Contents -- PART 1. DETONATIONS IN SOLIDS, LIQUIDS, AND GASES -- Stability of Detonation Waves at Low Pressures -- Spectrophotometric Analysis of Detonation Wave Structure -- Parametric Studies of Strong Gaseous Detonations -- Estimating Caloric State Behavior in Condensed-Phase Detonations -- Theoretical Treatment of the Detonation Behavior of Composite Propellants -- Detonations in Dilute Sprays -- PART 2. TWO-PHASE FLOW -- A. Two-Phase Nozzle Flow -- Perturbation Analysis of One-Dimensional Heterogeneous Flow in Rocket Nozzles -- Analysis of Two-Phase Flow in Supersonic Exhausts -- Flow of Gas-Particle Mixtures in Axially Symmetric Nozzles -- Particle Velocity Lag in Metalized Propellants -- Equilibrium Between Phases in Converging-Diverging Nozzles -- B. Stable and Unstable Combustion Processes in Liquid Fuel Rocket Engines -- Spray Combustion Model With Droplet Breakup: Analytical and Experimental Results -- Steady-State Combustion Measurements in a LOX/RP-1 Rocket Chamber and Related Spray Burning Analysis -- Application of Similarity Parameters for Correlating High Frequency Instability Behavior of Liquid Propellant Combustors -- Vibration and Combustion Investigation of the LR99 Engine -- Tangential Mode of Combustion Instability -- Contributors to Volume 6.
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Cover -- Title -- Copyright -- Propellants and Combustion Committee -- Liquid Rockets Committee -- Preface -- Contents -- PART 1. DETONATIONS IN SOLIDS, LIQUIDS, AND GASES -- Stability of Detonation Waves at Low Pressures -- Spectrophotometric Analysis of Detonation Wave Structure -- Parametric Studies of Strong Gaseous Detonations -- Estimating Caloric State Behavior in Condensed-Phase Detonations -- Theoretical Treatment of the Detonation Behavior of Composite Propellants -- Detonations in Dilute Sprays -- PART 2. TWO-PHASE FLOW -- A. Two-Phase Nozzle Flow -- Perturbation Analysis of One-Dimensional Heterogeneous Flow in Rocket Nozzles -- Analysis of Two-Phase Flow in Supersonic Exhausts -- Flow of Gas-Particle Mixtures in Axially Symmetric Nozzles -- Particle Velocity Lag in Metalized Propellants -- Equilibrium Between Phases in Converging-Diverging Nozzles -- B. Stable and Unstable Combustion Processes in Liquid Fuel Rocket Engines -- Spray Combustion Model With Droplet Breakup: Analytical and Experimental Results -- Steady-State Combustion Measurements in a LOX/RP-1 Rocket Chamber and Related Spray Burning Analysis -- Application of Similarity Parameters for Correlating High Frequency Instability Behavior of Liquid Propellant Combustors -- Vibration and Combustion Investigation of the LR99 Engine -- Tangential Mode of Combustion Instability -- Contributors to Volume 6.

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Electronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2024. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.

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