Print Email Facebook Twitter CAR 88: A method to calculate subsonic and supersonic, steady and unsteady, potential flow about complex configurations Title CAR 88: A method to calculate subsonic and supersonic, steady and unsteady, potential flow about complex configurations Author Hounjet, M.H.L. Institution National Aerospace Laboratory NLR Date 1988-10-07 Abstract A description is given of the method CAR88 for the calculation of steady and time-linearized unsteady subsonic and supersonic flow about complex 2-D and 3-D configurations. The method belongs to the category of the socalled panel methods. Results of applications in supersonic flow are shown which have been made to a 2-D oscillating flat plate, a 2-D double and single wedge airfoil, 3-D cones and to single and multiple interfering wing surface. Subject panel methods (fluid dynamics)computational fluid dynamicspotential flowunsteady flowsupersonic flowdata correlationintegral equationsaerodynamic configurationsthree dimensional flowwakespressure distributioncomputer systems performance To reference this document use: http://resolver.tudelft.nl/uuid:221e19e8-970d-44e0-9b69-43b759eb1658 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR 88154 U Part of collection Aerospace Engineering Reports Document type report Rights (c) 1988 National Aerospace Laboratory NLR Files PDF NLR_TR_88154_U.pdf 28.09 MB Close viewer /islandora/object/uuid:221e19e8-970d-44e0-9b69-43b759eb1658/datastream/OBJ/view