Author: Paul C. Setze Publisher: ISBN: Category : Boron Languages : en Pages : 46
Book Description
It was experimentally determined that the liquid boric oxide particles leaving a jet engine combustor, burning a boron-containing fuel, will have diameters of 1.0 x 10(exp -5) to 2.0 x 10(exp -5) centimeter. For this size range the particle heat-transfer and drag coefficients are essentially infinite. The results may be applied to any boron-containing fuel. Equations are developed that enable the calculation of the particle size-time history. A study of boric oxide deposition mechanisms is included, and suggestions for decreading deposition rates given.
Author: University of Michigan. Institute of Science and Technology. Ballistic Missile Radiation Analysis Center Publisher: ISBN: Category : Languages : en Pages : 418
Author: Paul C. Setze Publisher: ISBN: Category : A discussion of the effect of boric oxide deposits on jet engine performance is included Languages : en Pages : 43
Book Description
The deposition rate of boric oxide from a stream containing submicron particles was found experimentally to fit a molecular diffusion equation.
Author: S. S. Penner Publisher: Elsevier ISBN: 1483221296 Category : Technology & Engineering Languages : en Pages : 666
Book Description
The Chemistry of Propellants is a collection of papers and comments presented at the meeting on "The Chemistry of Propellants, held in Paris, France on June 8-12, 1959, organized by the AGARD Combustion and Propulsion Panel. This book is organized into six parts encompassing 25 chapters that serve as an introduction to the broad and important subject of propellant chemistry and propulsion applications. The first part deals with the sources, availability, and comparative costing of propulsion system. The second and third parts discuss the theoretical, thermodynamic, and experimental aspects of liquid and solid propellants. The fourth part examines the main problems concerning preparation, storage, and use of propellants for ramjet, while the fifth part looks into the factors leading to deposits in jet engines and some of the consequences of their existence. The sixth part covers the advantages of the high energy chemical propellants, including fluorine and hydrogen. Combustion and propulsion scientists and researchers will find this book beneficial.
Author: Paul C. Setze
Author: 
Author: University of Michigan. Institute of Science and Technology. Ballistic Missile Radiation Analysis Center
Author: 
Author: Paul C. Setze
Author: United States. Superintendent of Documents
Author: S. S. Penner
Author: United States. Superintendent of Documents
Author: 
Author: