TY  - RPRT
TI  - Advanced Methods for Aircraft Engine Thrust and Noise Benefits: Nozzle-Inlet Flow Analysis
AU  - Gilinsky, Mikhail
AU  - Morgan, Morris H.
AU  - Hardin, Jay C.
AU  - Mosiane, Lotlamoreng
AU  - Kaushal, Patel
AU  - Blankson, Isaiah M.
PY  - 2000
UR  - https://ntrs.nasa.gov/citations/20010012156
ID  - 20010012156
ER  -