Experimental Investigation Of Turbulent Step Induced Boundary Layer Separation At Mach Numbers 25 3 And 4
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Author | : Jerry S. Hahn |
Publisher | : |
Total Pages | : 39 |
Release | : 1969 |
Genre | : |
ISBN | : |
Download Experimental Investigation of Turbulent Step-induced Boundary-layer Separation at Mach Numbers 2.5, 3, and 4 Book in PDF, Epub and Kindle
An experimental investigation of turbulent separated boundary-layer flow was conducted using high forward-facing steps (with side plates) mounted on a flat plate at zero angle of attack. The tests were made at Mach numbers of 2.5, 3.0, and 4.0 for Reynolds numbers, based on the boundary-layer total thickness at the separation location, from 100,000 to 150,000. The effects of Mach number, step height and span, end plates, and step-face fairings were investigated. Data are presented graphically and in tabulations and include model surface pressures on the flat plate and on the face and top of selected steps, boundary-layer Mach number profiles, and selected oil dot photographs. (Author).
Author | : |
Publisher | : |
Total Pages | : 834 |
Release | : 1975 |
Genre | : |
ISBN | : |
Download NASA Technical Note 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 | : |
Publisher | : |
Total Pages | : 1074 |
Release | : 1979 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, Epub and Kindle
Author | : D. K. Patel |
Publisher | : |
Total Pages | : 68 |
Release | : 1975 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Theoretical Face Pressure and Drag Characteristics of Forward-facing Steps in Supersonic Turbulent Boundary Layers Book in PDF, Epub and Kindle
Author | : Richard D. Samuels |
Publisher | : |
Total Pages | : 82 |
Release | : 1967 |
Genre | : Skim friction (Aerodynamics) |
ISBN | : |
Download Experimental Investigation of the Turbulent Boundary Layer at a Mach Number of 6 with Heat Transfer at High Reynolds Numbers Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1338 |
Release | : 1969-04 |
Genre | : Science |
ISBN | : |
Download U. S. Government Research and Development Reports Book in PDF, Epub and Kindle
Author | : Shimer Zane Pinckney |
Publisher | : |
Total Pages | : 108 |
Release | : 1965 |
Genre | : Hypersonic planes |
ISBN | : |
Download Semiempirical Method for Predicting Effects of Incident-reflecting Shocks on the Turbulent Boundary Layer Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1336 |
Release | : 1969 |
Genre | : Science |
ISBN | : |
Download U.S. Government Research & Development Reports Book in PDF, Epub and Kindle
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 568 |
Release | : 1951 |
Genre | : Aeronautics |
ISBN | : |
Download Research Abstracts Book in PDF, Epub and Kindle