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Solution Of The Laminar Boundary Layer Of A Semi Infinite Flat Plate Given An Impulsive Change In Velocity And Temperature
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Book Synopsis Solution of the Laminar Boundary Layer of a Semi-infinite Flat Plate Given an Impulsive Change in Velocity and Temperature by : Michael David Bare
Download or read book Solution of the Laminar Boundary Layer of a Semi-infinite Flat Plate Given an Impulsive Change in Velocity and Temperature written by Michael David Bare and published by . This book was released on 1967 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt: Thesis (M.S.)
Book Synopsis The Solution of the Laminar-boundary-layer Equation for the Flat Plate for Velocity and Temperature Fields for Variable Physical Properties and for the Diffusion Field at High Concentration by : H. Shuh
Download or read book The Solution of the Laminar-boundary-layer Equation for the Flat Plate for Velocity and Temperature Fields for Variable Physical Properties and for the Diffusion Field at High Concentration written by H. Shuh and published by . This book was released on 1950 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: In connection with Pohlhausen's solution for the temperature field on the flat plate, a series of formulas were indicated by means of which the velocity and temperature field for variable physical characteristics can be computed by an integral equation and an iteration method based on it. With it, the following cases were solved: On the assumption that the viscosity simply varies with the temperature while the other fluid properties remain constant, the velocity and temperature field on the heated and cooled plate, respectively, was computed at the Prandtl numbers 12.5 and 100 (viscous fluids). A closer study of these two cases resulted in general relations: The calculations for a gas of Pr number 0.7 (air) were conducted on the assumption that all fluid properties vary with the temperature, and the velocities are low enough for the heat of friction to be discounted. The result was a thickening of the boundary layers, but no appreciable modification in shearing stress or heat-transfer coefficient.
Book Synopsis On the Incompressible Laminar Boundary Layer for Impulsive Motion of a Semi-infinite Flat Plate by : T. Akamatsu
Download or read book On the Incompressible Laminar Boundary Layer for Impulsive Motion of a Semi-infinite Flat Plate written by T. Akamatsu and published by . This book was released on 1966 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1974 with total page 620 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 1967 with total page 1058 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Solution of Compressible Laminar Boundary Layer Problems by a Finite Difference Method by : Donald Charles Baxter
Download or read book The Solution of Compressible Laminar Boundary Layer Problems by a Finite Difference Method written by Donald Charles Baxter and published by . This book was released on 1957 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Analysis of the Relaxation of Laminar Boundary Layer on a Flat Plate After Passage of an Interface with Application to Expansion-tube Flows by : Roop N. Gupta
Download or read book An Analysis of the Relaxation of Laminar Boundary Layer on a Flat Plate After Passage of an Interface with Application to Expansion-tube Flows written by Roop N. Gupta and published by . This book was released on 1972 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: The relaxation of the accelerating-gas boundary layer to the test-gas boundary layer over a flat plate in an expansion tube is analyzed. Several combinations of test gas and acceleration gas are considered. The problem is treated in two conically similar limits: (1) when the time lag between the arrival of the shock and the interface at the leading edge of the plate is very large, and (2) when this lag is negligible. The time-dependent laminar-boundary-layer equations of a binary mixture of perfect gases are taken as the flow-governing equations. This coupled set of differential equations, written in terms of the Lam-Crocco variables, has been solved by a line-relaxation finite-difference technique. The results presented include the Stanton number and the local skin-friction coefficient as functions of shock Mach number and the nondimensional distance-time variable. The results indicate that more than 95 percent of the test-gas boundary layer exists over a length, measured from the leading edge of the plate, equal to about three-tenths of the distance traversed by the interface in the free stream.
Book Synopsis Compressible Laminar Boundary Layer and Heat Transfer for Unsteady Motions of a Flat Plate by : Simon Ostrach
Download or read book Compressible Laminar Boundary Layer and Heat Transfer for Unsteady Motions of a Flat Plate written by Simon Ostrach and published by . This book was released on 1955 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: The laminar compressible boundary layer and heat transfer over an isothermal semi-infinite flat plate moving with a time-dependent velocity has been analyzed. First-order deviations from the quasi-steady velocity and temperature profiles and boundary-layer characteristics have been computed. For a plate oscillating about a steady velocity, it is shown that the maxima of skin-friction coefficient and local heat-transfer rate are out of phase with the phase velocity; the skin friction leads by angles not exceeding 45 degrees for permissible values of the frequency parameter, whereas the heat transfer is almost in phase with the plate velocity for very small Mach number but depends significantly on the Mach number, plate to stream temperature ratio, and frequency for higher-speed flows.
Book Synopsis Progress in Heat and Mass Transfer by :
Download or read book Progress in Heat and Mass Transfer written by and published by . This book was released on 1971 with total page 576 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Laminar Boundary Layer on a Flat Plate in Helium Using the Crocco Method by : K. M. Nicoll
Download or read book Investigation of the Laminar Boundary Layer on a Flat Plate in Helium Using the Crocco Method written by K. M. Nicoll and published by . This book was released on 1962 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Crocco method is used to solve the simultaneous differential equations governing the laminar boundary layer on a flat plate with zero pressure gradient, for gas properties corresponding to helium. Results are given for heat transfer rate, skin-friction coefficient, boundary layer thickness, recovery factor, and velocity and temperature profiles. The solution is compared with some experimental results for on particular case.
Download or read book CANCAM Proceedings written by and published by . This book was released on 1977 with total page 636 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Real-gas Study of Low-density Wedge-induced Laminar Separation on a Highly Cooled Blunt Flat Plate at M [infinity] by : John Benjamin Anders
Download or read book A Real-gas Study of Low-density Wedge-induced Laminar Separation on a Highly Cooled Blunt Flat Plate at M [infinity] written by John Benjamin Anders and published by . This book was released on 1968 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Laminar Velocity Profile in a Flat Plate Boundary Layer with Surface Roughness by : G. H. Hoffman
Download or read book The Laminar Velocity Profile in a Flat Plate Boundary Layer with Surface Roughness written by G. H. Hoffman and published by . This book was released on 1977 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt: The theory of Singh and lumley for the effect of surface roughness on a laminar boundary layer is applied to flow past a semi-infinite flat plate where the roughness is a randomly distributed small amplitude waviness characteristic of the manufacturing process. Distorted velocity profiles are calculated for a range of parameters and comparisons are made with results obtained by a phenomenological theory. Present results are nearly an order of magnitude smaller than those predicted by the phenomenological theory. (Author).
Download or read book Journal of Heat Transfer written by and published by . This book was released on 1968 with total page 542 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Solution of Laminar Boundary Layer Equations by the Finite Differnce Method by : Douglas Aircraft Company
Download or read book The Solution of Laminar Boundary Layer Equations by the Finite Differnce Method written by Douglas Aircraft Company and published by . This book was released on 1960 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book CANCAM 77 written by and published by . This book was released on 1977 with total page 642 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
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