Print Email Facebook Twitter An improved potential gradient method to calculate airloads on oscillating supersonic interfering surfaces Title An improved potential gradient method to calculate airloads on oscillating supersonic interfering surfaces Author Hounjet, M.H.L. Institution National Aerospace Laboratory NLR Date 1981-01-19 Abstract A description is given of a computationally inqjroved potential gradient method to calculate unsteady aerodynamic derivatives in supersonic flow. Results are presented and comparisons are made with results of existing methods and with experimental data for a fighter-type wing. To reference this document use: http://resolver.tudelft.nl/uuid:0b58cdd4-fe28-4149-88ad-679759365251 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR MP 81001 U Part of collection Aerospace Engineering Reports Document type report Rights (c)1981 National Aerospace Laboratory NLR Files PDF 81001.pdf 8.68 MB Close viewer /islandora/object/uuid:0b58cdd4-fe28-4149-88ad-679759365251/datastream/OBJ/view