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Modern Engineering for Design of Liquid Propellant Rocket Engines
Dieter K. Huzel,David H. Huang +1 more
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From the component design, to the subsystem design to the engine systems design, engine development and flight-vehicle application, this how-to text bridges the gap between basic physical and design principles and actual rocket-engine design as it's done in industry as mentioned in this paper.Abstract:
From the component design, to the subsystem design, to the engine systems design, engine development and flight-vehicle application, this how-to text bridges the gap between basic physical and design principles and actual rocket-engine design as it's done in industry. More than 470 illustrations and tables should make this book a must-read for advanced students and engineers active in all phases of engine systems design, development and application in industry and in government agencies.read more
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Liquid Fuels and Propellants for Aerospace Propulsion: 1903-2003
TL;DR: In this article, the authors describe the evolution of liquid fuels for aircraft and rockets as the engines and vehicles they fuel have undergone these signiµ cant increases in performance, and compare the performance of aircraft and vehicles with those of the space shuttle.
Book
Introduction to Turbomachinery
David Japikse,Nicholas Baines +1 more
TL;DR: In this paper, a conception reference record was created on 2005-11-18, modified on 2016-08-08 and was used for the construction of the turbines of the turbine.
Journal ArticleDOI
Supersonic Flow Separation with Application to Rocket Engine Nozzles
TL;DR: In this article, the increasing demand for higher performance in rocket launches promotes the development of nozzles with higher performance, which basically is achieved by increasing the expansion ratio of the nozzler.
Journal ArticleDOI
Large eddy simulation of laser ignition and compressible reacting flow in a rocket-like configuration
TL;DR: In this article, a simulation of a strong ignition sequence observed in a laboratory-scale single-injector rocket chamber ignited by a laser and fueled with gaseous oxygen and hydrogen is presented.
Journal ArticleDOI
Numerical analysis of regenerative cooling in liquid propellant rocket engines
Abdullah Ulas,E. Boysan +1 more
TL;DR: In this paper, the regenerative cooling of a liquid propellant rocket engine has been numerically simulated to operate on a LOX/kerosene mixture at a chamber pressure of 60 bar with 300 kN thrust and kerosene is considered as the coolant.