TY  - RPRT
TI  - Developing and utilizing an Euler computational method for predicting the airframe/propulsion effects for an aft-mounted turboprop transport. Volume 1: Theory document
AU  - Chen, H. C.
AU  - Yu, N. Y.
PY  - 1991
UR  - https://ntrs.nasa.gov/citations/19910014805
ID  - 19910014805
ER  -