A review is presented of the accomplishment of the near term objectives of developing an analysis system and optimization methods during the first year of the NASA Langley High Speed Airframe Integration Research (HiSAIR) project. The characteristics of a Mach 3 HSCT transport have been analyzed utilizing the newly developed process. In addition to showing more detailed information about the aerodynamic and structural coupling for this type of vehicle, this exercise aided in further refining the data requirements for the analysis process.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Preliminary results from the High Speed Airframe Integration Research project



    Publication date :

    1992-02-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Preliminary results from the High Speed Airframe Integration Research project

    COEN, PETER / SOBIESZCZANSKI-SOBIESKI, JAROSLAW / DOLLYHIGH, SAMUEL | AIAA | 1992


    Airframe/Engine Integration

    A. Ferri | NTIS | 1972


    Intake-Airframe Integration

    L. E. Surber | NTIS | 1988


    Engine-airframe integration

    Nicholson, L.F. | Engineering Index Backfile | 1957


    Airframe engine integration

    NATO, Advisory Group for Aerospace Research and Development | TIBKAT | 1972