@chfenger
Aerospace software
Osculating cone method for waverider design
A simple one-dimensional combustor analysis routine in FORTRAN
Method Of Characteristics (MOC) routines for flow flied analysis, maximum thrust nozzle design and supersonic wind tunnel nozzle design.
One dimensional method that simulates dual-mode Scramjet isolator-combustor in Fortran
Main atmospheric properties of the US Standard Atmosphere, 1962.
Two dimensional Riemann problem
