Examples Of The Effects Of Shock Induced Boundary Layer Separation In Transonic Flight
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Author | : H. H. Pearcey |
Publisher | : |
Total Pages | : 58 |
Release | : 1954 |
Genre | : |
ISBN | : |
Download Examples of the Effects of Shock-induced Boundary-layer Separation in Transonic Flight Book in PDF, Epub and Kindle
Author | : Herbert Harry Pearcey |
Publisher | : |
Total Pages | : 58 |
Release | : 1967 |
Genre | : |
ISBN | : |
Download Examples of the Effects of Shock-induced Boundary-layer Separation in Transonic Flight Book in PDF, Epub and Kindle
Author | : H. H. Pearcey |
Publisher | : |
Total Pages | : 57 |
Release | : 1967 |
Genre | : Shock waves |
ISBN | : |
Download Examples of the Effects of Shock-induce Boundary-layer Separation in Transonic Flight Book in PDF, Epub and Kindle
Author | : H.H. Pearcey |
Publisher | : |
Total Pages | : 57 |
Release | : 1967 |
Genre | : |
ISBN | : |
Download Examples of the Effects of Shock-indiced Boundary-layer Separation in Transonic Flight Book in PDF, Epub and Kindle
Author | : Holger Babinsky |
Publisher | : Cambridge University Press |
Total Pages | : 481 |
Release | : 2011-09-12 |
Genre | : Technology & Engineering |
ISBN | : 1139498649 |
Download Shock Wave-Boundary-Layer Interactions Book in PDF, Epub and Kindle
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.
Author | : Jones F. Cahill |
Publisher | : |
Total Pages | : 92 |
Release | : 1968 |
Genre | : Mach number |
ISBN | : |
Download Flight Text Investigation of Transonic Shock-boundary Layer Phenomena Book in PDF, Epub and Kindle
Author | : Eugene S. Love |
Publisher | : |
Total Pages | : 702 |
Release | : 1955 |
Genre | : Aerodynamic load |
ISBN | : |
Download Pressure Rise Associated with Shock-induced Boundary-layer Separation Book in PDF, Epub and Kindle
Some recent contributions to the problem of shock-induced separation of the boundary layer are examined, and additional analytical and experimental results are presented. The probable ranges of pressure rises and flow deflections associated with separation are indicated. Consideration is given to the effects of Mach number, adverse pressure gradient, and Reynolds number for laminar boundary layers and to the effects of Mach number, Reynolds number, and ratio of sepcific heats for turbulent boundary layers.
Author | : H. H. Pearcey |
Publisher | : |
Total Pages | : |
Release | : 1955 |
Genre | : |
ISBN | : |
Download Some Effects of Shock-induced Separation of Turbulent Boundary Layers in Transonic Flow Past Aerofoils Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 0 |
Release | : 1967 |
Genre | : |
ISBN | : |
Download Effects of Initial Turbulent Boundary Layer on Shock-induced Separation in Transonic Flow Book in PDF, Epub and Kindle
Author | : Coleman duP. Donaldson |
Publisher | : |
Total Pages | : 38 |
Release | : 1950 |
Genre | : Aerofoils |
ISBN | : |
Download Investigation of a Simple Device for Preventing Separation Due to Shock and Boundary-layer Interaction Book in PDF, Epub and Kindle
Results are presented of a preliminary investigation of vortex generators introduced into the region of boundary layer to increase the turbulent mixing, in an attempt to prevent separation due to boundary-layer and shock interaction. Prevention of such separation and some of its adverse effects up to Mach numbers ahead of the shock of the order of 1.4 appears possible by means of this simple device. Preliminary flight tests show that this method is effective in controlling shock-induced separation on the wing of an airplane at high speed.