Accession Number : AD0691143
Title : CALCULATION OF COMPRESSIBLE FLOWFIELDS ABOUT SHARP-NOSED SYMMETRIC AIRFOILS AT ZERO ANGLE OF ATTACK.
Descriptive Note : Aeroballistics technical note,
Corporate Author : GENERAL DYNAMICS/CONVAIR SAN DIEGO CALIF
Personal Author(s) : Magnus,R. J. ; Gallaher,W. H.
Report Date : 07 DEC 1967
Pagination or Media Count : 34
Abstract : A computer program was written for the calulation of compressible flows about sharp-nosed symmetric airfoils at zero angle of attack. Starting from an arbitrary initial guess of the flowfield, the time-dependent equations are numerically integrated using a two-step finite-difference scheme. Appropriate boundary conditions are maintained at the borders of the spatial field and the asymptotic, for large time, solution is taken to represent steady flow. An example is presented and plans to extend the method to treat blunt-nosed lifting airfoils are discussed. (Author)
Descriptors : (*AIRFOILS, *COMPRESSIBLE FLOW), FLOW FIELDS, ANGLE OF ATTACK, LIFT, NUMERICAL ANALYSIS, EQUATIONS OF MOTION
Subject Categories : Aerodynamics
Distribution Statement : APPROVED FOR PUBLIC RELEASE