In present work a test rig for cold flow test experiments on linear aerospike nozzles has been designed at Politecnico di Torino. CFD analysis was performed on 2D and 3D aerospike models in order to understand which would be the better inlet nozzle geometry able to work with the designed test-rig mass flow. A time resolved pressure measurement system for the study of flow instabilities has been designed and its dynamic response evaluated.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Cold Gas Measurement System for Linear Aerospike Nozzles




    Publication date :

    2022-06-27


    Size :

    1902377 byte





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Numerical investigation on linear aerospike nozzles

    Dai, Wuye / Liu, Yu / Zhang, Zhengke et al. | AIAA | 2001


    Performance analysis of linear clustered aerospike nozzles

    Changhui, W. / Yu, L. / Lizi, Q. | British Library Online Contents | 2004


    COLD GAS EXPERIMENTS ON LINEAR, THRUST-VECTORED AEROSPIKE NOZZLES THROUGH SECONDARY INJECTION

    Sieder-Katzmann, Jan / Propst, Martin / Tajmar, Martin et al. | TIBKAT | 2020


    Flowfield Characterization of Linear Aerospike Nozzles (AIAA 2014-0551)

    Takahashi, H. / Tomioka, S. / Tomita, T. et al. | British Library Conference Proceedings | 2014


    Experimental and numerical studies on aerospike nozzles

    Liu, Yu / Zhang, Zhengke / Dai, Wuye et al. | AIAA | 1999