Print Email Facebook Twitter A surface flow solution and stability derivates for bodies of revolution in complex supersonic flow. Part I. Theory and some representative results Title A surface flow solution and stability derivates for bodies of revolution in complex supersonic flow. Part I. Theory and some representative results Author Ohman, L.H. Institution National Research Council Canada, National Aeronautical Establishment, High Speed Aerodynamjcs Section Date 1964-11-30 Abstract A method of determining the surface flow velocities for arbitrary pointed bodies of revolution in complex supersonic flow, j.e., flow due te constant incidence, constant pitching velocity and constant lateral acceleration, has been derived and a corresponding numerical procedure developed . The method is based on a solution suggested by M. J. Lighthill for the symmetrical flow case. Good correspondence between results of the present methad with available " exact", and exact linear results for cones has been found for the range 0 to 1 of the similarity parameter ßτ. Using the exact isentropic pressure - velocity relation, expressions for the limiting value of the pressure coefficient derivatives as the independent To reference this document use: http://resolver.tudelft.nl/uuid:a1a7b52b-5535-43a2-87ee-c55bb147ae23 Publisher National Research Council Canada Access restriction Campus only Source National Research Council Aeronautical Report LR 418 Part of collection Aerospace Engineering Reports Document type report Rights (c)1964 National Research Council Canada Files PDF LR-418.pdf 5.97 MB Close viewer /islandora/object/uuid:a1a7b52b-5535-43a2-87ee-c55bb147ae23/datastream/OBJ/view