Investigation Of A Thick Laminar Boundary Layer In A Supersonic Nozzle
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Experimental and Numerical Investigation of Boundary-layer Development and Transition on the Walls of a Mach 5 Nozzle
Author | : William D. Harvey |
Publisher | : |
Total Pages | : 92 |
Release | : 1975 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
The Effect of Blade-section Thickness Ratios on the Aerodynamic Characteristics of Related Full-scale Propellers at Mach Numbers Up to 0.65
Author | : A. J. Eggers |
Publisher | : |
Total Pages | : 284 |
Release | : 1953 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Shock Wave-Boundary-Layer Interactions
Author | : Holger Babinsky |
Publisher | : Cambridge University Press |
Total Pages | : 481 |
Release | : 2011-09-12 |
Genre | : Technology & Engineering |
ISBN | : 1139498649 |
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.
Torsional Stiffness of Thin-walled Shells Having Reinforcing Cores and Rectangular, Triangular, Or Diamond Cross Section
Author | : Alberta Y. Alksne |
Publisher | : |
Total Pages | : 338 |
Release | : 1957 |
Genre | : Aerodynamic load |
ISBN | : |
Research Review
Author | : United States. Air Force. Office of Aerospace Research |
Publisher | : |
Total Pages | : 346 |
Release | : 1969 |
Genre | : |
ISBN | : |