TY  - RPRT
TI  - A computer program for the calculation of the flow field including boundary layer effects for mixed-compression inlets at angle of attack
AU  - Vadyak, J.
AU  - Hoffman, J. D.
PY  - 1982
UR  - https://ntrs.nasa.gov/citations/19830002796
ID  - 19830002796
ER  -