Hanson, Perry Warden2014-03-142014-03-141953-03-02etd-11072012-040148http://hdl.handle.net/10919/45514The various parametric curves in reference 6 were found to be very difficult to read accurately, Therefore, a set of more convenient curves of the various quantities and parameters for the lower range of Mach numbers has been plotted and is included for the reader's ready reference.52 leavesBTDapplication/pdfenIn CopyrightLD5655.V855 1953.H368Aerodynamics, SupersonicAn engineering evaluation of the continuity method for predicting the form and location of detached shock waves for two-dimensional flowThesishttp://scholar.lib.vt.edu/theses/available/etd-11072012-040148/