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Elsevier

Detonation and Two-Phase Flow

  • 1 Edición - 1 de enero de 1962
  • Última edición
  • Editor: S Penner
  • Idioma: Inglés

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… Leer más

Descripción

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.

Índice


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

Detalles del producto

  • Edición: 1
  • Última edición
  • Publicado: 12 de noviembre de 2012
  • Idioma: Inglés

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