TY  - RPRT
TI  - An approximate viscous shock layer technique for calculating nonequilibrium hypersonic flows about blunt-nosed bodies
AU  - Cheatwood, F. M.
AU  - Dejarnette, F. R.
PY  - 1992
UR  - https://ntrs.nasa.gov/citations/19920043702
ID  - 19920043702
ER  -