TY  - RPRT
TI  - Scramjet Engine Flowpath Development for the Hyper-X Mach 10 Flight Test
AU  - Rogers, R. C.
AU  - Shih, A. T.
AU  - Hass, N. E.
PY  - 2005
UR  - https://ntrs.nasa.gov/citations/20050234608
ID  - 20050234608
ER  -