Wall shear in strongly retarded and separated compressible turbulent boundary layers
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Engineering topics
Publications and source records attributed to Murphy, J. D..
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The purpose of this paper is to show that most existing methods for the calculation of fluid flows can be interpreted as special applications of a single mathematical formalism. This formalism, called the generalized Galerkin method, then provides a single conceptual framework for comparing various methods in terms of convergence and accuracy. The method is presented in sufficient mathematical detail to permit its interpretation as a projection in function space. In order to demonstrate the basic thesis, finite difference, finite element, strip integral, and classical integral methods of boundary layer theory are developed by application of the method.
Interaction regions created by the impingement of full span, externally generated, shock waves on a nozzle wall boundary layer were investigated. Incident shock strength was varied to produce unseparated, incipient, and fully separated flow fields. Significant departures from two-dimensionality were observed over the entire range of shock strengths tested and were identified with sidewall and corner boundary layer effects. However, comparisons of present centerline results with published two-dimensional data, obtained under similar test conditions and geometrical constraints, showed excellent agreement (e.g., incipient separation pressure levels, wall pressure distributions, free-interaction, and scale of the interaction region). This raises some question concerning the degree of two-dimensionality achieved in these previous investigations.
Critical evaluation of analytic methods of predicting interaction between laminar boundary layer and impinging shock waves
Prediction methods for boundary layer and flow field characteristics in shock wave-boundary layer interaction
Laminar and turbulent boundary layer interactions with externally generated shock waves
Integral relations method efficiency and accuracy in solving incompressible turbulent boundary layer equations, noting acceptability for turbulent flows with small wake components
Analytical model for oblique shock wave interaction with turbulent boundary layer
Method of integral relations applied to solution of incompressible turbulent boundary layer equations
Afterbody heating by Mercury spacecraft during reentry determined from skin temperatures
Positive ion collection by spherical Langmuir probes
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Stagnation point velocity and pressure distribution over heat-sink shielded reentry vehicle to test boundary layer heat transfer theories
Blunt body reentry vehicle aerodynamic heating determination