TY  - RPRT
TI  - A theory for base pressures in multi-nozzle rocket configurations.
AU  - Abbud, K. A.
AU  - Lamb, J. P.
AU  - Lenzo, C. S.
PY  - 1969
UR  - https://ntrs.nasa.gov/citations/19690054762
ID  - 19690054762
ER  -