Print Email Facebook Twitter Demonstration of an automated CFD system for three-dimensional flow simulations Title Demonstration of an automated CFD system for three-dimensional flow simulations Author van der Burg, J.W. Maseland, J.E.J. Hagmeijer, R. de Cock, K.M.J. Institution National Aerospace Laboratory NLR Date 1995-04-04 Abstract In this paper the capabilities of an automated CFD system which is currently available at NLR are demonstrated. Transonic flow around the AS28G wing/body configuration and hypersonic flow through a generic three-dimensional mixed-compression airbreathing inlet are simulated. An assessment of the level of automation of the current CFD-system is made. The problem-turnaround time lies within the order of a week for both applications Subject Aircraft configurationsComputational gridsComputational fluid dynamicsComputer aided designGraphical user interfaceHypersonic flowIntake systemsNumerical flow visualizationRun time (computers)Three dimensional modelsTransonic flowTriangulation To reference this document use: http://resolver.tudelft.nl/uuid:7474fd02-3e8d-41a1-8824-3e82a07ff60f Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR Technical Publication TP 95120 U Part of collection Aerospace Engineering Reports Document type report Rights (c)1994 National Aerospace Laboratory NLR Files campus only