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  • Aircraft Propulsion and Power  (1)
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    Multidisciplinary Analysis of a Hypersonic Engine (2002)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: This paper describes implementation of a technique used to obtain a high fidelity fluid-thermal-structural solution of a combined cycle engine at its scram design point. Single-discipline simulations are insufficient here since interactions from other disciplines are significant. Using off-the-shelf, validated solvers for the fluid, chemistry, thermal, and structural solutions, this approach couples together their results to obtain consistent solutions.
    Keywords: Aircraft Propulsion and Power
    Type: NASA/TM-2002-211971 , NAS 1.15:211971 , E-13614 , AIAA Paper 2002-5127 , 11th International Conference on Space Planes and Hypersonic Systems and Technologies; Sep 29, 2002 - Oct 04, 2002; Orleans; France
    Format: application/pdf
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