Download Full eBooks in PDF
Structurally Compliant Rocket Engine Combustion Chamber Experimental And Analytical Validation Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Structurally Compliant Rocket Engine Combustion Chamber Experimental And Analytical Validation book. This book definitely worth reading, it is an incredibly well-written.
Author : Robert S. Jankovsky
Publisher : Unknown
Page : 20 pages
File Size : 50,8 Mb
Release : 1994
Category : Materials
ISBN : NASA:31769000447493
Author : Anonim
Publisher : Unknown
Page : 724 pages
File Size : 50,8 Mb
Release : 1996
Category : Mechanics, Applied
ISBN : UIUC:30112046051295
Author : Anonim
Publisher : Unknown
Page : 464 pages
File Size : 49,9 Mb
Release : 1995
Category : Aeronautics
ISBN : MINN:30000011064593
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author : Nikolaus A. Adams,Wolfgang Schröder,Rolf Radespiel,Oskar J. Haidn,Thomas Sattelmayer,Christian Stemmer,Bernhard Weigand
Publisher : Springer Nature
Page : 409 pages
File Size : 51,5 Mb
Release : 2020-10-26
Category : Technology & Engineering
ISBN : 9783030538477
This open access book presents the findings of Collaborative Research Center Transregio 40 (TRR40), initiated in July 2008 and funded by the German Research Foundation (DFG). Gathering innovative design concepts for thrust chambers and nozzles, as well as cutting-edge methods of aft-body flow control and propulsion-component cooling, it brings together fundamental research undertaken at universities, testing carried out at the German Aerospace Center (DLR) and industrial developments from the ArianeGroup. With a particular focus on heat transfer analyses and novel cooling concepts for thermally highly loaded structures, the book highlights the aft-body flow of the space transportation system and its interaction with the nozzle flow, which are especially critical during the early phase of atmospheric ascent. Moreover, it describes virtual demonstrators for combustion chambers and nozzles, and discusses their industrial applicability. As such, it is a timely resource for researchers, graduate students and practitioners.
Author : S.N. Atluri,G. Yagawa,Thomas A. Cruse
Publisher : Springer Science & Business Media
Page : 3181 pages
File Size : 51,5 Mb
Release : 2013-11-11
Category : Technology & Engineering
ISBN : 9783642796548
AI!, in the earlier conferences (Tokyo, 1986; Atlanta, 1988, Melbourne, 1991; and Hong Kong, 1992) the response to the call for presentations at ICES-95 in Hawaii has been overwhelming. A very careful screening of the extended abstracts resulted in about 500 paper being accepted for presentation. Out of these, written versions of about 480 papers reached the conference secretariat in Atlanta in time for inclusion in these proceedings. The topics covered at ICES-95 range over the broadest spectrum of computational engineering science. The editors thank the international scientific committee, for their advice and encouragement in making ICES-95 a successful scientific event. Special thanks are expressed to the International Association for Boundary Elements Methods for hosting IABEM-95 in conjunction with ICES-95. The editors here express their deepest gratitude to Ms. Stacy Morgan for her careful handling of a myriad of details of ICES-95, often times under severe time constraints. The editors hope that the readers of this proceedings will find a kaleidoscopic view of computational engineering in the year 1995, as practiced in various parts of the world. Satya N. Atluri Atlanta, Georgia, USA Genki Yagawa Tokyo,Japan Thomas A. Cruse Nashville, TN, USA Organizing Committee Professor Genki Yagawa, University of Tokyo, Japan, Chair Professor Satya Atluri, Georgia Institute of Technology, U.S.A.
Author : Anonim
Publisher : Unknown
Page : 1732 pages
File Size : 48,8 Mb
Release : 1995
Category : Government publications
ISBN : UIUC:30112063915075
Author : Satya N. Atluri,Genki Yagawa
Publisher : Unknown
Page : 1368 pages
File Size : 47,7 Mb
Release : 1997
Category : Engineering mathematics
ISBN : UVA:X004113873
Author : Anonim
Publisher : Unknown
Page : 1450 pages
File Size : 42,6 Mb
Release : 2024-06-02
Category : Government publications
ISBN : WISC:89117117994
Author : Anonim
Publisher : Unknown
Page : 840 pages
File Size : 45,9 Mb
Release : 1994
Category : Science
ISBN : MINN:30000005965987
Author : Anonim
Publisher : Unknown
Page : 1686 pages
File Size : 44,8 Mb
Release : 199?
Category : Electronic
ISBN : MSU:31293017238712
Author : John R. Szuch
Publisher : Unknown
Page : 44 pages
File Size : 53,5 Mb
Release : 1968
Category : Liquid propellants
ISBN : UIUC:30112101601166
Author : John E. Dalgleish,Adelbert O. Tischler
Publisher : Unknown
Page : 20 pages
File Size : 45,6 Mb
Release : 1953
Category : Aeronautics
ISBN : UOM:39015086431874
Experiments have been conducted with a jacketed rocket combustion chamber that was fabricated by hydraulic forming from sheet metal. Rocket combustion chambers made by this method have been used successfully. Runs with these combustion chambers have been made at over-all heat-transfer rates of 2.5 Btu per square inch per second with water cooling and also the ammonia as a regenerative coolant.
Author : Rene Nardi Rezende
Publisher : SAE International
Page : 158 pages
File Size : 50,8 Mb
Release : 2018-11-15
Category : Technology & Engineering
ISBN : 9780768093322
The great engineering achievement required to overcome most of the challenges and obstacles that prevented turning rocket design from art into science took place in Europe and the United States between the 1930s and the 1950s. With the vast majority of the engines currently in operation developed in the “pre-computer” age, there are new opportunities to update the design methodologies using technology that can now handle highly complex calculations fast. The space sector with an intense focus on efficiency is driving the need for updating, adapting or replacing the old modeling practices with new tools capable of reducing the volume of resources and the time required to complete simulations and analysis. This book presents an innovative parametric model applicable to the project of some elements of the liquid rocket thrust chamber with the level of detail and accuracy appropriate to the preliminary design phase. It addresses the operating characteristics and dimensioning of some thrust chamber elements through a set of equations and parameters, which include thrust or propellant characteristics. The model degree of sophistication was adjusted to the requirements of the Project Life Cycle Phase B, while also enabling quick analysis of new configurations from changes in initial project parameters.
Author : Zhen-Guo Wang
Publisher : John Wiley & Sons
Page : 392 pages
File Size : 52,8 Mb
Release : 2016-08-29
Category : Technology & Engineering
ISBN : 9781118890028
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 : Anonim
Publisher : Unknown
Page : 492 pages
File Size : 42,6 Mb
Release : 1994
Category : Aeronautics
ISBN : MINN:31951P00691495X