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.


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    Title :

    Flow Processes in Overexpanded Chemical Rocket Nozzles. Part 2: Side Loads by a Symmetric Separation Stroemungsvorgaenge Beim Betrieb Ueberexpandierter Duesen Chemischer Raketentriebwerke. Teil 2: Seitenkraefte durch Unsymmetrische Abloesung


    Contributors:

    Publication date :

    1973


    Size :

    60 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English