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Laminar Hypersonic Boundary Layer Slip Flow Past A Semi Infinite Flat Plate With Displacement Thickness Interaction
Download Laminar Hypersonic Boundary Layer Slip Flow Past A Semi Infinite Flat Plate With Displacement Thickness Interaction full books in PDF, epub, and Kindle. Read online Laminar Hypersonic Boundary Layer Slip Flow Past A Semi Infinite Flat Plate With Displacement Thickness Interaction ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Laminar Hypersonic Boundary-layer Slip Flow Past a Semi-infinite Flat Plate with Displacement Thickness Interaction by : Rong-Shuang Wang
Download or read book Laminar Hypersonic Boundary-layer Slip Flow Past a Semi-infinite Flat Plate with Displacement Thickness Interaction written by Rong-Shuang Wang and published by . This book was released on 1969 with total page 212 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1976 with total page 1072 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wedge-induced Laminar-boundary-layer Separation on a Flat Plate in Low-density, Hypervelocity Flow by : John Benjamin Anders
Download or read book Wedge-induced Laminar-boundary-layer Separation on a Flat Plate in Low-density, Hypervelocity Flow written by John Benjamin Anders and published by . This book was released on 1970 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Approximate Method for Estimating the Incompressible Laminar Boundary-layer Characteristics on a Flat Plate in Slipping Flow by : Coleman duP. Donaldson
Download or read book An Approximate Method for Estimating the Incompressible Laminar Boundary-layer Characteristics on a Flat Plate in Slipping Flow written by Coleman duP. Donaldson and published by . This book was released on 1949 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: An approximate method is presented for the estimation of the properties of the incompressible laminar boundary layer on a flat plate in the slip-flow regime using Kármán's momentum method. These results are compared with results for a normal boundary layer at the same Reynolds number to bring out the characteristics of a slip boundary layer. A simple criterion for the importance of slip is presented.
Book Synopsis Effects of Leading-edge Bluntness and Ramp Deflection Angle on Laminar Boundary-layer Separation in Hypersonic Flow by : James Courtland Townsend
Download or read book Effects of Leading-edge Bluntness and Ramp Deflection Angle on Laminar Boundary-layer Separation in Hypersonic Flow written by James Courtland Townsend and published by . This book was released on 1966 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Viscous Hypersonic Flow by : William H. Dorrance
Download or read book Viscous Hypersonic Flow written by William H. Dorrance and published by Courier Dover Publications. This book was released on 2017-05-22 with total page 353 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Integral Methods in Compressible Laminar Boundary Layers and Their Application to Hypersonic Pressure Interactions by : Yat-Yung Chan
Download or read book Integral Methods in Compressible Laminar Boundary Layers and Their Application to Hypersonic Pressure Interactions written by Yat-Yung Chan and published by . This book was released on 1965 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Boundary-layer Displacement Effects in Air at Mach Numbers of 6.8 and 9.6 by : Mitchel H. Bertram
Download or read book Boundary-layer Displacement Effects in Air at Mach Numbers of 6.8 and 9.6 written by Mitchel H. Bertram and published by . This book was released on 1959 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA SP. written by and published by . This book was released on 1970 with total page 1166 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Laminar and Turbulent Boundary Layers Interacting with Externally Generated Shock Waves by : Earl C. Watson
Download or read book Investigation of Laminar and Turbulent Boundary Layers Interacting with Externally Generated Shock Waves written by Earl C. Watson and published by . This book was released on 1969 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt: Laminar and turbulent boundary layer interactions with externally generated shock waves.
Book Synopsis A Computer Study of Hypersonic Laminar Boundary-layer/shock-wave Interaction Using the Time-dependent Compressible Navier-Stokes Equations by : B. K. Hodge
Download or read book A Computer Study of Hypersonic Laminar Boundary-layer/shock-wave Interaction Using the Time-dependent Compressible Navier-Stokes Equations written by B. K. Hodge and published by . This book was released on 1976 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents the results of an investigation of hypersonic laminar boundary-layer/shock-wave interactions using the method of MacCormack to solve the time-dependent compressible Navier-Stokes equations. Comparisons of the numerical solutions with experimental data were made to ascertain the validity of the numerical method and to identify regions of anomalous behavior. The algorithm gave good results when applied to hypersonic laminar interactions that caused either small or no separated regions and marginal performance when applied to hypersonic laminar interactions having large regions of separated flow. The extents of the separated regions in interactions having large regions of separated flow were underpredicted when compared with experimental data. The predicted wall heat-transfer rates exhibited the correct qualitative trend but not the experimentally measured quantitative values. Consideration of the effects of needed stabilizing terms as well as grid resolution suggests inadequate mesh spacing in the longitudinal direction as the cause of the aforementioned anomalies. If inadequate mesh spacing (and the corresponding lack of support for every term of the Navier-Stokes equations) is a prime cause of the cited discrepancies between the numerical results and the experimental data, then the needed reduction of several orders of magnitude in delta x, would increase CPU time and core storage requirements to untenable levels. (Author).
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1963 with total page 1196 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis On the Instability of Hypersonic Flow Past a Flat Plate by : Institute for Computer Applications in Science and Engineering
Download or read book On the Instability of Hypersonic Flow Past a Flat Plate written by Institute for Computer Applications in Science and Engineering and published by . This book was released on 1990 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: The instability of hypersonic boundary-layer flows over flat plates is considered. The viscosity of the fluid is taken to be governed by Sutherland's law, which gives a much more accurate representation of the temperature dependence of fluid viscosity at hypersonic speeds than Chapmans's approximate linear law; although at lower speeds the temperature variation of the mean state is less pronounced so that the Chapman law can be used with some confidence. Attention is focussed on the so-called vorticity mode of instability of the viscous hypersonic boundary layer. The instability of the hypersonic boundary layer is non-interactive. The vorticity mode of instability of this flow operates on a significantly different lengthscale than that obtained if a Chapman viscosity law is assumed. The growth rate predicted by a linear viscosity law overestimates the size of the growth rate by O (M-sq). Next, the development of the vorticity mode as the wavenumber decreases is described, and it is shown that acoustic modes emerge when the wavenumber has decreased from it's O(1) initial value to O (M to the -3/2 power). (jhd).
Book Synopsis On Local Flat-plate Similarity in the Hypersonic Boundary Layer by : Franklin Kingston Moore
Download or read book On Local Flat-plate Similarity in the Hypersonic Boundary Layer written by Franklin Kingston Moore and published by . This book was released on 1960 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Comprehensive Dissertation Index, 1861-1972: Engineering: general and aeronautical by : Xerox University Microfilms
Download or read book Comprehensive Dissertation Index, 1861-1972: Engineering: general and aeronautical written by Xerox University Microfilms and published by . This book was released on 1973 with total page 906 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Study of Flow Separation in Regions of Shock Wave-boundary Layer Interaction in Hypersonic Flow by : Michael S. Holden
Download or read book A Study of Flow Separation in Regions of Shock Wave-boundary Layer Interaction in Hypersonic Flow written by Michael S. Holden and published by . This book was released on 1975 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes a theoretical and experimental investigation of the properties of attached and separated regions of shock wave-laminar boundary layer interacting in the strong interaction regime. The flow is studied over a flat plate-wedge compression surface in the high Mach number, low Reynolds number regime where the interaction between the viscous and inviscid regions over the basic flat plate is strong and of fundamental importance to the problem. The theoretical analysis treats the development of the viscous layer and its interaction with the external inviscid stream, using an integral representation for the boundary layer equations. A complementary experimental study investigated the flow over a flat plate-wedge compression surface for a range of free-stream Reynolds number and Mach number conditions in the strong interaction regime.
Book Synopsis Axisymmetric Laminar Boundary Layers with Very Large Transverse Curvature by : Jay M. Solomon
Download or read book Axisymmetric Laminar Boundary Layers with Very Large Transverse Curvature written by Jay M. Solomon and published by . This book was released on 1967 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt: The compressible axisymmetric laminar boundary layer is considered for very large values of the transverse curvature parameter (roughly proportional to the ratio of the Mangler value of the boundary layer displacement thickness to the local cross-sectional radius of the body). Asymptotic expansions are constructed using the method of inner-outer expansions and verified by comparison with exact numerical similarity solutions. Both finite and hypersonic Mach number inviscid flow conditions are considered. The principal results are asymptotic formulas for skin friction, heat transfer, and boundary layer displacement thickness. Existing expansions, obtained by Wei, are found to be incorrect. The viscous pressure interaction near the vertex of a pointed axisymmetric body is treated within the framework of boundary layer theory and a tangent-cone approximation. (Author).
