Nonsimilar solutions for laminar film condensation of liquid metals
Liquid metals vapor drag and electromagnetic fields effects on laminar film condensation, using finite difference method
Denny, V. E.↗
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Results for “Laminarization”
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Laminar film condensation on plane and axisymmetric bodies in nonuniform gravity
Laminar film condensation thickness and Nusselt number on arbitrary axisymmetric bodies in nonuniform gravity
Dhir, V.↗
Recirculation patterns in confined laminar jet mixing
Recirculation patterns in coaxial steady laminar mixing of homogeneous jets in confined tube, solving Navier-Stokes equations
Lavan, Z.↗
Laminar flow between two infinite disks, one rotating and the other stationary
Constant property fluid laminar flow between rotating and stationary infinite disks for limiting Reynolds numbers based on gap width
Reshotko, E.↗
Laminar incompressible flow past a circulation- controlled circular lifting rotor
Prandtl first order boundary layer equations for two dimensional laminar incompressible flow past circulation controlled circular lifting rotor
Plotkin, A.↗
Laminar boundary layers with large wall heating and flow acceleration
Laminar boundary layers with large wall heating and flow acceleration, considering heat transfer parameter increase
Back, L. H.↗
Laminar wave-train structure of collisionless magnetic slow shocks
Collisionless magnetic slow shocks laminar wave train structure, using two-fluid hydromagnetics with ion cyclotron radius dispersion
Coroniti, F. V.↗
Analytical and experimental investigation of laminar mixing of confined heterogeneous jets
Recirculating cells and entrance conditions influence on confined heterogeneous jets laminar mixing, measuring velocity and concentration profiles
Lavan, Z.↗
Experimental study of effects of laminar boundary layers on chemical-kinetic measurements in a shock tube
Laminar boundary layers effect on chemical-kinetic measurements in shock tube, applying correction by computer program for subsonic diffuser
Belles, F. E.↗
Development of an approximation analysis for the laminar boundary layer behind a moving shock wave
Approximation analysis for laminar two dimensional boundary layer behind plane shock wave moving over infinite flat plate
Abbott, D. E.↗
The flow of a laminar, incompressible jet along a parabola
Plane laminar incompressible jet flow along parabola with no external stream, using second order boundary layer theory
Plotkin, A.↗
Numerical solution of the interaction of a shock wave with a laminar boundary layer
Shock wave interaction with laminar boundary layer on flat plate using modified Lax-Wendroff difference technique
Maccormack, R. W.↗
Effects of laminar and turbulent boundary layer buildup in shock tubes upon chemical rate measurements
Predicted flow nonuniformities due to laminar and turbulent boundary layer buildup in shock tubes, studying effects on dissociation rates of bromine in argon mixture
Warshay, M.↗
Interfacial shear factors for laminar film boiling from a vertical surface
Forced flow laminar film boiling heat transfer coefficients from vertical surface in terms of interfacial shear at liquid-vapor interface
Baumeister, K. J.↗
Computation of laminar heat transfer from gaseous plasmas in electromagnetic fields
Heat transfer analysis procedure is presented for two-temperature gaseous plasma. Analysis is based on laminar flow of singly-ionized, quasineutral plasma with variable properties. Sheath analysis is described for species in accelerating field, decelerating field, emitted from wall, and recombining at wall.
Bose, T. K.↗
Calculation of compressible nonadiabatic boundary layers in laminar, transitional and turbulent flow by the method of integral relations
A computer program was developed to do the calculations for two-dimensional or axisymmetric configurations from low speeds to hypersonic speeds with arbitrary streamwise pressure, temperature, and Mach number distributions. Options are provided for obtaining initial conditions either from experimental information or from a theoretical similarity solution. The transition region can be described either by an arbitrary distribution of intermittency or by a function based on Emmons' probability theory. Correlations were developed for use in estimating the parameters of the theoretical intermittency function. Correlations obtained from other sources are used for estimating the transition point. Comparisons were made between calculated and measured boundary layer quantities for laminar, transitional, and turbulent flows on flat plates, cones, cone flares, and a waisted body of revolution. Excellent agreement was obtained between the present theory and two other theories based on the method of finite differences. The intermittency required to reproduce some experimental heat transfer results in hypersonic flow was found to be quite different from the theoretical function. It is suggested that the simple probability theory of Emmons may not be valid for representing the intermittency of hypersonic transitional boundary layers and that the program could be useful as a tool for detailed study of the intermittency of the transition region.
Kuhn, G. D.↗
Experimental Investigation of Laminar Gas Jet Diffusion Flames in Zero Gravity
An experimental program was conducted to study the burning of laminar gas jet diffusion flames in a zero-gravity environment. The tests were conducted in a 2.2-Second-Zero-Gravity Facility and were a part of a continuing effort investigating the effects of gravity on basic combustion processes. The photographic results indicate that steady state gas jet diffusion flames existed in zero gravity but they were geometrically quite different than their normal-gravity counterparts. Methane-air flames were found to be approximately 50 percent longer and wider in zero gravity than in normal gravity.
Cochran, Thomas H.↗
On the calculation of three dimensional laminar boundary layer flows
An approximation which reduces the computation of three dimensional, laminar, compressible, boundary layer equations to the problem of solving two dimensional type boundary layer equations is presented. A comparison of this method with a fully three dimensional boundary layer calculation is provided.
Fillo, J. A.↗