PSE Analysis of Reacting Hypersonic Boundary Layer Transition PDF Download
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Author: Heath B. Johnson
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: Heath B. Johnson
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: C.-L. Chang
Publisher:
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Category :
Languages : en
Pages :
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Author: Spencer Sherwin
Publisher: Springer Nature
ISBN: 3030679020
Category : Computers
Languages : en
Pages : 809
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This volume comprises the carefully revised papers of the 9th IUTAM Symposium on Laminar-Turbulent Transition, held at the Imperial College, London, UK, in September 2019. The papers focus on the leading research in understanding transition to turbulence, which is a challenging topic of fluid mechanics and arises in many modern technologies as well as in nature. The proceedings are of interest for researchers in fluid mechanics and industry who have to handle these types of problems, such as in the aeronautical sector.
Author: William H. Dorrance
Publisher: Courier Dover Publications
ISBN: 0486822583
Category : Technology & Engineering
Languages : en
Pages : 353
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Designed for advanced undergraduate and graduate courses in modern boundary-layer theory, this frequently cited work offers a self-contained treatment of theories for treating laminar and turbulent boundary layers of reacting gas mixtures. 1962 edition.
Author: Melissa L. Manning
Publisher:
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Category :
Languages : en
Pages :
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Author: Heath Bradley Johnson
Publisher:
ISBN:
Category :
Languages : en
Pages : 264
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Author: Heath B. Johnson
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Category :
Languages : en
Pages :
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Author: Xiaolin Zhong
Publisher:
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Category : Aerodynamics, Hypersonic
Languages : en
Pages : 56
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 33
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The goal of this research is to study the laminar turbulent transition and other transient flow phenomena of 3-D chemically reacting hypersonic boundary layers by direct numerical simulation (DNS) and by linear stability analysis. The research in the report period was focused on developing new numerical methods for such studies and studying several fundamental transient hypersonic flow phenomena. First, several new efficient and high-order accurate numerical methods for DNS of 3-D hypersonic reacting boundary layers and for computing unsteady hypersonic flows with complex shock interactions were developed. These new methods were developed in order to overcome difficulties associated with the direct numerical simulation of hypersonic flows. Second, several studies on the stability phenomena of hypersonic boundary layers over blunt leading edges both by direct numerical simulation and by linear stability analyses were performed. Also completed were extensive numerical studies on real gas effects on a steady shock/boundary layer interaction and a self-sustained unsteady shock-shock interference heating flows. Third, the effects of using Burnett equations for rarefied hypersonic flow computations were investigated. With the completion of the bulk of work on the development of new numerical methods for complex hypersonic flow simulation, the DNS studies are currently being extended to 3-D hypersonic boundary layer transition over elliptic cross section cones.
Author:
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ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 92
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