Print Email Facebook Twitter Application of the method of integral relations (MIR) to transonic airfoil problems. Part I: Inviscid supercritical flow over symmetric airfoils at zero angle of atack Title Application of the method of integral relations (MIR) to transonic airfoil problems. Part I: Inviscid supercritical flow over symmetric airfoils at zero angle of atack Author Tai, Tsze C. Faculty Mechanical, Maritime and Materials Engineering Department Marine and Transport Technology Research group Ship Hydromechanics and Structures Date 1970 Subject resistance & propulsion To reference this document use: http://resolver.tudelft.nl/uuid:6186d295-ca5b-4069-a6d5-f5e8ecd50706 Report number NSRDC Report 3424 Source Naval Ship Research and Development Center, Washington DC, USA, Department of Aerodynamics, Research and Development Report 3424 Part of collection Maritime Archive Document type report Files PDF 16859.pdf 1.54 MB Close viewer /islandora/object/uuid:6186d295-ca5b-4069-a6d5-f5e8ecd50706/datastream/OBJ/view