Detonation and Two-Phase Flow

Detonation and Two-Phase Flow

1st Edition - January 1, 1962

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  • Editor: S Penner
  • eBook ISBN: 9780323153188

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Description

Progress in Astronautics and Rocketry, Volume 6: Detonation and Two-Phase Flow compiles technical papers presented at the ARS Propellants, Combustion, and Liquid Rockets Conference held in Palm Beach, Florida on April 26-28, 1961. This book provides an excellent illustration of research and development on a selected group of problems relating to detonations, two-phase nozzle flow, and combustion in liquid fuel rocket engines. This volume is divided into two parts. Part 1 covers the entire range of physical conditions under which detonation may be initiated or sustained, such as high explosives, solid propellants, liquid sprays, and gases. Experimental and theoretical studies are also discussed, including the significant progress of the basic phenomena involved in transition from deflagration to detonation, and nature of stable detonations in dilute sprays and other systems. The perennial problems associated with high frequency instabilities in liquid fuel rocket engines are considered in Part 2. This publication is valuable to students and investigators working in the field of propulsion research and development.

Table of Contents


  • Propellants and Combustion Committee

    Liquid Rockets Committee

    Preface

    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

Product details

  • No. of pages: 380
  • Language: English
  • Copyright: © Academic Press 1962
  • Published: January 1, 1962
  • Imprint: Academic Press
  • eBook ISBN: 9780323153188

About the Editor

S Penner

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