TY  - RPRT
TI  - Computation of aircraft component flow fields at transonic Mach numbers using a three-dimensional Navier-Stokes algorithm
AU  - Shrewsbury, George D.
AU  - Vadyak, Joseph
AU  - Schuster, David M.
AU  - Smith, Marilyn J.
PY  - 1989
UR  - https://ntrs.nasa.gov/citations/19890011562
ID  - 19890011562
ER  -