Liquid Rocket Engine Turbines
Author : S. B. Macaluso
Publisher :
Page : 164 pages
File Size : 49,37 MB
Release : 1974
Category : Liquid propellant rockets
ISBN :
Author : S. B. Macaluso
Publisher :
Page : 164 pages
File Size : 49,37 MB
Release : 1974
Category : Liquid propellant rockets
ISBN :
Author : National Aeronautics and Space Administration
Publisher :
Page : 147 pages
File Size : 50,84 MB
Release : 1974
Category :
ISBN :
Author : Jack D. Mattingly
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 0 pages
File Size : 13,78 MB
Release : 2005
Category : Aircraft gas-turbines
ISBN : 9781563477782
This text provides an introduction to gas turbine engines and jet propulsion for aerospace or mechanical engineers. The text is divided into four parts: introduction to aircraft propulsion; basic concepts and one-dimensional/gas dynamics; parametric (design point) and performance (off-design) analysis of air breathing propulsion systems; and analysis and design of major gas turbine engine components (fans, compressors, turbines, inlets, nozzles, main burners, and afterburners). Design concepts are introduced early (aircraft performance in introductory chapter) and integrated throughout. Written with extensive student input on the design of the book, the book builds upon definitions and gradually develops the thermodynamics, gas dynamics, and gas turbine engine principles.
Author : Dieter K. Huzel
Publisher : AIAA
Page : 452 pages
File Size : 11,82 MB
Release : 1992
Category : Liquid propellant rocket engines
ISBN : 9781600864001
Author :
Publisher :
Page : 132 pages
File Size : 12,20 MB
Release : 1978
Category : Jet pumps
ISBN :
Author : Andrew M. Brown
Publisher : Springer Nature
Page : 177 pages
File Size : 10,18 MB
Release : 2023-02-14
Category : Technology & Engineering
ISBN : 3031182073
This is the first Structural Dynamics book focused on this indispensable aspect of liquid rocket engine design. This book begins by reviewing basic concepts in Structural Dynamics, including the free and forced response of SDOF and MDOF systems, along with some discussion of how numerical solutions are generated. The book then moves to a discussion of specific applications of these techniques in LREs, progressing from component level (turbomachinery and combustion devices), up through engine system models, and finally to integration with a launch vehicle. Clarifies specific topics including the Campbell and SAFE Diagrams for resonance identification in turbomachinery, the complications of component analysis in the pump side due to a host of complication factors such as acoustic/structure interaction, the "side-loads" fluid/structure interaction problem in overexpanded rocket nozzles, and competing methods for generation overall engine system interface loads. Includes specific examples for illustration while closing with rotordynamic analysis, dynamic data analysis, and vibroacoustics.
Author : Mark L. Dranovsky
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 352 pages
File Size : 27,48 MB
Release : 2007
Category : Technology & Engineering
ISBN : 9781563479212
This is the first book in the literature to cover the development and testing practices for liquid rocket engines in Russia and the former Soviet Union.Combustion instability represents one of the most challenging probelms in the development of propulsion engines. A famous example is the F-1 engines for the first stage of the Saturn V launch vehicles in the Apollo project. More than 2000 full engine tests and a vast number of design modifications were conducted to cure the instability problem.This book contains first-hand information about the testing and development practices for treating liquid rocket combustion-instability problems in Russia and the former Soviet Union. It covers more than 50 years of research, with an emphasis placed on the advances made since 1970.The book was prepared by a former R&D director of the Research Institute of Chemical Engineering, NIICHIMMASH, the largest liquid rocket testing center in the world, and has been carefully edited by three well-known experts in the field.
Author : L. K. Severud
Publisher :
Page : 140 pages
File Size : 43,51 MB
Release : 1972
Category : Liquid propellant rockets
ISBN :
Author : George Paul Sutton
Publisher : AIAA
Page : 936 pages
File Size : 23,55 MB
Release : 2006
Category : Technology & Engineering
ISBN : 9781563476495
Liquid propellant rocket engines have propelled all the manned space flights, all the space vehicles flying to the planets or deep space, virtually all satellites, and the majority of medium range or intercontinental range ballistic missiles.
Author : Erian A. Baskharone
Publisher : Cambridge University Press
Page : 599 pages
File Size : 12,72 MB
Release : 2006-07-31
Category : Science
ISBN : 0521858100
This book is intended for advanced undergraduate and graduate students in mechanical and aerospace engineering taking a course commonly called Principles of Turbomachinery or Aerospace Propulsion. The book begins with a review of basic thermodynamics and fluid mechanics principles to motive their application to aerothermodynamics and real-life design issues. This approach is ideal for the reader who will face practical situations and design decisions in the gas turbine industry. The text is fully supported by over 200 figures, numerous examples, and homework problems.