Print Email Facebook Twitter ARSPNSC: A method to calculate subsonic steady and unsteady potential flow about complex configurations Title ARSPNSC: A method to calculate subsonic steady and unsteady potential flow about complex configurations Author Hounjet, M.H.L. Institution National Aerospace Laboratory NLR Date 1986-12-01 Abstract A new method ARSPSC is described for the calculation of steady and time-linearized unsteady subsonic potential flow about complex 2-D and 3-D configurations. The method belongs to the category of the so-called panel methods. Applications have been made to a 2-D oscillating flat plate, a 2-D multi-component airfoil with oscillating flap and a 3-D fighter-type wing. Subject Panel methodsWing oscillationsFluid DynamicsSuctionWakesUnsteady flowPotential flowSubsonic flowSteady flowAerodynamic dragPressure distributionAlgorithmsFinite volume methodIntegral Equations To reference this document use: http://resolver.tudelft.nl/uuid:02c184b3-57bb-4188-8c95-8ccef6363847 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR 86122 U Part of collection Aerospace Engineering Reports Document type report Rights (c)1986 National Aerospace Laboratory NLR Files campus only