TY  - RPRT
TI  - Reentry heating and flow fields for Space Shuttle Orbiter at high angle of attack.
AU  - Rochelle, W. C.
AU  - Roberts, B. B.
AU  - D'Attorre, L.
AU  - Vogenitz, F. W.
PY  - 1972
UR  - https://ntrs.nasa.gov/citations/19720041582
ID  - 19720041582
ER  -