Print Email Facebook Twitter Calculations of pressure distributions on two-dimensional wings oscillating at low frequencies in high subsonic and low supersonic flow Title Calculations of pressure distributions on two-dimensional wings oscillating at low frequencies in high subsonic and low supersonic flow Author Zwaan, R.J. Institution National Aerospace Laboratory NLR Date 1970-06-01 Abstract Using asymptotic matching techniques methods are developed to calculate pressure distributions on two-dimensional wings oscillating at low frequencies in high subsonic and low supersonic flow. Special attention is given to a wing with oscillating control surface. Results for such a configuration are compared with experiments. To reference this document use: http://resolver.tudelft.nl/uuid:98df5c64-a92c-434f-ba0f-f8466fcb51a0 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR 70047 U Part of collection Aerospace Engineering Reports Document type report Rights (c) 1970 National Aerospace Laboratory NLR Files PDF NLR_TR_70047_U.pdf 78.79 MB Close viewer /islandora/object/uuid:98df5c64-a92c-434f-ba0f-f8466fcb51a0/datastream/OBJ/view