Two Phase Flow Combustion Modelling of a Ducted Rocket
Author | : R. A. Stowe |
Publisher | : |
Total Pages | : |
Release | : 2001 |
Genre | : |
ISBN | : |
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Author | : R. A. Stowe |
Publisher | : |
Total Pages | : |
Release | : 2001 |
Genre | : |
ISBN | : |
Author | : S Penner |
Publisher | : Elsevier |
Total Pages | : 381 |
Release | : 2012-12-02 |
Genre | : Technology & Engineering |
ISBN | : 0323153186 |
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.
Author | : S. S. Penner |
Publisher | : |
Total Pages | : 388 |
Release | : 1962 |
Genre | : Science |
ISBN | : |
Author | : Gao Bo |
Publisher | : |
Total Pages | : |
Release | : 1999 |
Genre | : |
ISBN | : |
Author | : American Rocket Society |
Publisher | : |
Total Pages | : 368 |
Release | : 1962 |
Genre | : Combustion |
ISBN | : 9781563478550 |
Author | : Zhen-Guo Wang |
Publisher | : John Wiley & Sons |
Total Pages | : 509 |
Release | : 2016-05-17 |
Genre | : Technology & Engineering |
ISBN | : 1118890051 |
This book concentrates on modeling and numerical simulations of combustion in liquid rocket engines, covering liquid propellant atomization, evaporation of liquid droplets, turbulent flows, turbulent combustion, heat transfer, and combustion instability. It presents some state of the art models and numerical methodologies in this area. The book can be categorized into two parts. Part 1 describes the modeling for each subtopic of the combustion process in the liquid rocket engines. Part 2 presents detailed numerical methodology and several representative applications in simulations of rocket engine combustion.
Author | : E. Daniel |
Publisher | : |
Total Pages | : |
Release | : 2000 |
Genre | : |
ISBN | : |
Author | : National Aeronautics and Space Administration (NASA) |
Publisher | : Createspace Independent Publishing Platform |
Total Pages | : 170 |
Release | : 2018-07-17 |
Genre | : |
ISBN | : 9781723087325 |
This final report summarizes the major findings on the subject of 'Fundamental Phenomena on Fuel Decomposition and Boundary-Layer Combustion Processes with Applications to Hybrid Rocket Motors', performed from 1 April 1994 to 30 June 1996. Both experimental results from Task 1 and theoretical/numerical results from Task 2 are reported here in two parts. Part 1 covers the experimental work performed and describes the test facility setup, data reduction techniques employed, and results of the test firings, including effects of operating conditions and fuel additives on solid fuel regression rate and thermal profiles of the condensed phase. Part 2 concerns the theoretical/numerical work. It covers physical modeling of the combustion processes including gas/surface coupling, and radiation effect on regression rate. The numerical solution of the flowfield structure and condensed phase regression behavior are presented. Experimental data from the test firings were used for numerical model validation. Kuo, Kenneth K. and Lu, Yeu-Cherng and Chiaverini, Martin J. and Johnson, David K. and Serin, Nadir and Risha, Grant A. and Merkle, Charles L. and Venkateswaran, Sankaran Marshall Space Flight Center HYBRID ROCKET ENGINES; PROPULSION SYSTEM PERFORMANCE; DUCTED ROCKET ENGINES; COMBUSTION PHYSICS; BOUNDARY LAYERS; FUEL COMBUSTION; TEST FACILITIES; FLOW DISTRIBUTION; SOLID PROPELLANTS; REACTION KINETICS...
Author | : K. C. Schadow |
Publisher | : |
Total Pages | : 7 |
Release | : 1981 |
Genre | : |
ISBN | : |
Experiments with gaseous fuels to establish the base for the multiphase fuel tests were completed for the axisymmetric-coaxial flow fields. Radial and axial profiles of pressure, velocity, species concentration and temperature were determined. Agreement between measured values (velocity and temperature) and computer predictions was, in general, reasonably good. Experiments to determine axial and radial temperature profiles with boron particle-laden fuels were started. (Author).
Author | : |
Publisher | : |
Total Pages | : 516 |
Release | : 2001 |
Genre | : Airplanes |
ISBN | : |