Base flow field investigation on the S-2 stage
Modified computer program using finite difference method for calculating base flow field and dissipation for Saturn S-2 stage
Dattorre, L.↗
Engineering topics
Thommen, H. U.
Publications and source records attributed to Thommen, H. U..
An inviscid analysis of the plume created by multiple rocket engines and a comparison with available Schlieren data. I - Calculation of multiple rocket engine exhaust plumes by the method of characteristics. II - A finite difference method.
Multiple rocket engine exhaust plumes calculated by method of characteristics and finite difference and compared with schlieren data
ROCKET EXHAUST↗
Inviscid analysis of the plume created by multiple rocket engines. Part II - Description of the computer programs
Computer program for calculation of single jet and five jet interaction regimes associated with multiple rocket engines
ROCKET ENGINE↗