Heterogeneous combustion a selection of technical papers based mainly on the American Institute of Aeronautics and Astronautics Heterogeneous Combustion Conference held at Palm Beach, Florida, December 11-13, 1963.
Clasificación: | Libro Electrónico |
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Autor Corporativo: | |
Otros Autores: | |
Formato: | Electrónico Congresos, conferencias eBook |
Idioma: | Inglés |
Publicado: |
New York,
Academic Press,
1964.
|
Colección: | Progress in astronautics and aeronautics ;
v. 15. |
Temas: | |
Acceso en línea: | Texto completo |
Tabla de Contenidos:
- Cover
- Title
- Copyright
- The Propellants and Combustion Committee
- Preface
- Table of Contents
- I. Combustion and Ignition of Metals
- Techniques for the Study of Combustion of Beryllium and Aluminum Particles
- Study of Quenched Aluminum Particle Combustion
- Spectroscopic Investigation of Metal Combustion
- Vapor-Phase Diffusion Flames in the Combustion of Magnesium and Aluminum: I. Analytical Developments
- Vapor-Phase Diffusion Flames in the Combustion of Magnesium and Aluminum: II. Experimental Observations in Oxygen Atmospheres
- Vapor-Phase Diffusion Flames in the Combustion of Magnesium and Aluminum: III. Experimental Observations in Carbon Dioxide AtmospheresAnalysis of a Dilute Diffusion Flame Maintained by Heterogenous Reaction
- Combustion of Elemental Boron with Fluorine
- Oxidation of Graphite, Molybdenum, and Tungsten at 1000° to 1600°C
- Combustion of Pyrolytic Boron Nitride
- Combustion and Disintegration of Zirconium Hydride
- Uranium Fuel Rods during Atmospheric Re-Entry
- II. High-Energy Propellant Combustion
- A Brief Review on the Combustion of Boron Hydrides
- Characteristics of Diborane FlamesMechanism and Chemical Inhibition of the Diborane-Oxygen Reaction.
- Oxidation of Diethyldiborane
- Reaction of Pentaborane and Hydrazine and the Structure of the Adduct
- Mechanism of Pyrolysis of Aluminum AlkyIs
- Inhibition of Afterburning by Metal Compounds
- III. Effect of Aerodynamics on Heterogeneous Combustion
- Introductory Considerations on Hybrid Rocket Combustion
- Fundamentals of Hybrid Boundary-Layer Combustion
- Combustion during Perpendicular Flow
- Research in Hybrid Combustion
- A Porous Plug Burner Technique for the Study of Composite Solid Propellant Deflagration on a Fundamental Level and Its Application to Hybrid Rocket PropulsionProduction of Trace Species in Boundary Layers
- Laminar Boundary-Layer Wedge Flows with Evaporation and Combustion
- IV. Condensation
- Homogeneous Nucleation in Condensation
- Homogeneous Nucleation from Simple and Complex Systems
- Condensation Phenomena in Nozzles
- Water Vapor Condensation as an Explanation for the Great Apparent Radiance of Sun-Lit High-Altitude Rocket Exhaust Plumes