Accession Number : AD0782479
Title : Asymptotic Solution for Supersonic Viscous Flow Past a Compression Corner.
Descriptive Note : Technical rept.,
Corporate Author : OHIO STATE UNIV COLUMBUS DEPT OF AERONAUTICAL AND ASTRONAUTICAL ENGINEERING
Personal Author(s) : Jenson,R. ; Burggraf,O. R. ; Rizzetta,D. P.
Report Date : JUL 1974
Pagination or Media Count : 10
Abstract : The boundary-layer flow is forced to separate from the wall when a downstream compressive disturbance of sufficient magnitude is encountered. The correct asymptotic mathematical structure for such a viscous-inviscid interacting flow has been developed by Stewartson and Williams in their paper on self-induced separation. A numerical solution of these asymptotic equations of motion is presented here for the case of separation produced in supersonic flow past a compression ramp. The flow through separation ahead of the corner agrees with the Stewartson and Williams solution, but the reattachment of the separated flow onto the ramp is of different nature than the downstream flow in their case. (Author)
Descriptors : *Supersonic flow, *Viscous flow, Compression, Separation, Numerical analysis
Subject Categories : Numerical Mathematics
Distribution Statement : APPROVED FOR PUBLIC RELEASE