Shock-Induced Separated Structures in Symmetric Corner Flows
Author : D. D'Ambrosio
Publisher :
Page : 38 pages
File Size : 19,94 MB
Release : 1995
Category :
ISBN :
Shock Wave-Boundary-Layer Interactions
Author : Holger Babinsky
Publisher : Cambridge University Press
Page : 481 pages
File Size : 41,9 MB
Release : 2011-09-12
Category : Technology & Engineering
ISBN : 1139498649
Book Description
Shock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place.
Unsteady Effects of Shock Wave induced Separation
Author : Piotr Doerffer
Publisher : Springer Science & Business Media
Page : 350 pages
File Size : 43,69 MB
Release : 2010-11-25
Category : Technology & Engineering
ISBN : 3642030041
Book Description
This volume contains description of experimental and numerical results obtained in the UFAST project. The goal of the project was to generate experiment data bank providing unsteady characteristics of the shock boundary layer interaction. The experiments concerned basic-reference cases and the cases with application of flow control devices. Obtained new data bank have been used for the comparison with available simulation techniques, starting from RANS, through URANS, LES and hybrid RANS-LES methods. New understanding of flow physics as well as ability of different numerical methods in the prediction of such unsteady flow phenomena will be discussed.
New Results in Numerical and Experimental Fluid Mechanics II
Author : Wolfgang Nitsche
Publisher : Springer Science & Business Media
Page : 550 pages
File Size : 15,71 MB
Release : 2013-11-11
Category : Mathematics
ISBN : 3663109011
Book Description
This volume contains the papers of the 11th Symposium of the AG STAB (German Aerospace Aerodynamics Association). In this association those scientists and engineers from universities, research-establishments and industry are involved, who are doing research and project work in numerical and experimental fluid mechanics and aerodynamics for aerospace and other applications. Many of the contributions are giving results from the "Luftfahrtforschungsprogramm der Bundesregierung (German Aeronautical Research Programme). Some of the papers report on work sponsored by the Deutsche Forschungsgemeinschaft, DFG, which also was presented at the symposium. The volume gives a broad overview over the ongoing work in this field in Germany.
Shock-Induced Separated Structures in Symmetric Corner Flows
Author : National Aeronautics and Space Adm Nasa
Publisher :
Page : 38 pages
File Size : 18,99 MB
Release : 2018-10-19
Category :
ISBN : 9781728916781
Book Description
Three-dimensional supersonic viscous laminar flows over symmetric corners are considered in this paper. The characteristic features of such configurations are discussed and an historical survey on the past research work is presented. A new contribution based on a numerical technique that solves the parabolized form of the Navier-Stokes equations is presented. Such a method makes it possible to obtain very detailed descriptions of the flowfield with relatively modest CPU time and memory storage requirements. The numerical approach is based on a space-marching technique, uses a finite volume discretization and an upwind flux-difference splitting scheme (developed for the steady flow equations) for the evaluation of the inviscid fluxes. Second order accuracy is reached following the guidelines of the ENO schemes. Different free-stream conditions and geometrical configurations are considered. Primary and secondary streamwise vortical structures embedded in the boundary layer and originated by the interaction of the latter with shock waves are detected and studied. Computed results are compared with experimental data taken from literature. DAmbrosio, Domenic and Marsilio, Roberto Langley Research Center NAS1-19480; RTOP 505-90-52-01...
Basic Research and Technologies for Two-Stage-to-Orbit Vehicles
Author : Dieter Jacob
Publisher : John Wiley & Sons
Page : 683 pages
File Size : 11,65 MB
Release : 2006-03-06
Category : Technology & Engineering
ISBN : 3527605509
Book Description
Focusing on basic aspects of future reusable space transportation systems and covering overall design, aerodynamics, thermodynamics, flight dynamics, propulsion, materials, and structures, this report presents some of the most recent results obtained in these disciplines. The authors are members of three Collaborative Research Centers in Aachen, Munich and Stuttgart concerned with hypersonic vehicles. A major part of the research presented here deals with experimental and numerical aerodynamic topics ranging from low speed to hypersonic flow past the external configuration and through inlet and nozzle. Mathematicians and engineers jointly worked on aspects of flight mechanics like trajectory optimization, stability, control and flying qualities. Structural research and development was predominantly coupled to the needs for high temperature resistant structures for space vehicles.
NASA Technical Memorandum
Author :
Publisher :
Page : 176 pages
File Size : 22,97 MB
Release : 1996
Category : Aeronautics
ISBN :
Book Description
26th AIAA Fluid Dynamics Conference
Author :
Publisher :
Page : 478 pages
File Size : 33,3 MB
Release : 1995
Category : Fluid dynamics
ISBN :
Book Description
Progress in Hybrid RANS-LES Modelling
Author : Song Fu
Publisher : Springer Science & Business Media
Page : 508 pages
File Size : 38,82 MB
Release : 2012-08-14
Category : Technology & Engineering
ISBN : 3642318185
Book Description
The present book contains contributions presented at the Fourth Symposium on Hybrid RANS-LES Methods, held in Beijing, China, 28-30 September 2011, being a continuation of symposia taking place in Stockholm (Sweden, 2005), in Corfu (Greece, 2007), and Gdansk (Poland, 2009). The contributions to the last two symposia were published as NNFM, Vol. 97 and Vol. 111. At the Beijing symposium, along with seven invited keynotes, another 46 papers (plus 5 posters) were presented addressing topics on Novel turbulence-resolving simulation and modelling, Improved hybrid RANS-LES methods, Comparative studies of difference modelling methods, Modelling-related numerical issues and Industrial applications.. The present book reflects recent activities and new progress made in the development and applications of hybrid RANS-LES methods in general.
Unsteady Supersonic Combustion
Author : Mingbo Sun
Publisher : Springer Nature
Page : 380 pages
File Size : 21,10 MB
Release : 2020-04-14
Category : Technology & Engineering
ISBN : 9811535957
Book Description
This book describes the unsteady phenomena needed to understand supersonic combustion. Following an initial chapter that introduces readers to the basic concepts in and classical studies on unsteady supersonic combustion, the book highlights recent studies on unsteady phenomena, which offer insights on e.g. interactions between acoustic waves and flames, flow dominating instability, ignition instability, flame flashback, and near-blowout-limit combustion. In turn, the book discusses in detail the fundamental mechanisms of these phenomena, and puts forward practical suggestions for future scramjet design.
