TY  - RPRT
TI  - Experimental investigation of a large-scale, two-dimensional, mixed-compression inlet system: Internal performance and drag at transonic conditions, free stream Mach equals 0.6 to 1.28
AU  - Wong, N. D.
AU  - Anderson, W. E.
PY  - 1973
UR  - https://ntrs.nasa.gov/citations/19730023196
ID  - 19730023196
ER  -