Author: Michael HoldenPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 88
Book Description
Separated Flow Studies at Hypersonic Speeds: Separated flows over axisymmetric spiked bodies
Author: Michael HoldenPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 88
Book Description
NASA Technical Note
Author: Separation of Flow
Author: Paul K. ChangPublisher: Elsevier
ISBN: 1483181286
Category : Technology & Engineering
Languages : en
Pages : 800
Book Description
Interdisciplinary and Advanced Topics in Science and Engineering, Volume 3: Separation of Flow presents the problem of the separation of fluid flow. This book provides information covering the fields of basic physical processes, analyses, and experiments concerning flow separation. Organized into 12 chapters, this volume begins with an overview of the flow separation on the body surface as discusses in various classical examples. This text then examines the analytical and experimental results of the laminar boundary layer of steady, two-dimensional flows in the subsonic speed range. Other chapters consider the study of flow separation on the two-dimensional body, flow separation on three-dimensional body shape and particularly on bodies of revolution. This book discusses as well the analytical solutions of the unsteady flow separation. The final chapter deals with the purpose of separation flow control to raise efficiency or to enhance the performance of vehicles and fluid machineries involving various engineering applications. This book is a valuable resource for engineers.
Technical Abstract Bulletin
Author: 28th International Symposium on Shock Waves
Author: Konstantinos KontisPublisher: Springer Science & Business Media
ISBN: 3642256880
Category : Science
Languages : en
Pages : 860
Book Description
The University of Manchester hosted the 28th International Symposium on Shock Waves between 17 and 22 July 2011. The International Symposium on Shock Waves first took place in 1957 in Boston and has since become an internationally acclaimed series of meetings for the wider Shock Wave Community. The ISSW28 focused on the following areas: Blast Waves, Chemically Reacting Flows, Dense Gases and Rarefied Flows, Detonation and Combustion, Diagnostics, Facilities, Flow Visualisation, Hypersonic Flow, Ignition, Impact and Compaction, Multiphase Flow, Nozzle Flow, Numerical Methods, Propulsion, Richtmyer-Meshkov, Shockwave Boundary Layer Interaction, Shock Propagation and Reflection, Shock Vortex Interaction, Shockwave Phenomena and Applications, as well as Medical and Biological Applications. The two Volumes contain the papers presented at the symposium and serve as a reference for the participants of the ISSW 28 and individuals interested in these fields.
Flow-field Investigation for Large-angle Cones with Short Spikes at a Mach Number of 9.6
Author: W. Frank StaylorPublisher:
ISBN:
Category : Blunt bodies
Languages : en
Pages : 42
Book Description
Wind-tunnel Study of Oscillating Flow-induced Surface Pressures on a Tension-cone Geometry Model
Author: Frank P. BaltakisPublisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 62
Book Description
Oscillating flow about a spiked body in a supersonic stream has been investigated in a wind tunnel at Mach 5 at free-stream unit Reynolds numbers of 2,500,000 to 20,000,000 per foot using fast-response pressure transducers, accelerometers and schlieren movie cameras. A tension-cone-type model with replaceable nosetips of two different lengths and two different surface roughnesses was used.
Aerodynamic Investigation of Sharp Cone-cylinder Spikes on 120 ̊blunted Cones at Mach Numbers of 3.00, 4.50, and 6.00
Author: Robert J. McGheePublisher:
ISBN:
Category : Blunt bodies
Languages : en
Pages : 50
Book Description
Author: 
Author: