Flow processes in overexpanded chemical rocket nozzles. Part 2: Side loads due to asymmetric separation

R. H. Schmucker

NASA Technical Reports Server (NASA) · 1984 · 16 citations · 0 references

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Abstract

Methods for measuring the lateral forces, occurring as a result of asymmetric nozzle flow separation, are discussed. The effect of some parameters on the side load is explained. A new method was developed for calculation of the side load. The values calculated are compared with side load data of the J-2 engine. Results are used for predicting side loads of the space shuttle main engine.