NASAs Environmentally Responsible Aviation (ERA) Project explores enabling technologies to reduce aviations impact on the environment. One research challenge area for the project has been to study advanced airframe and engine integration concepts to reduce community noise and fuel burn. In order to achieve this, complex wind tunnel experiments at both the NASA Langley Research Centers (LaRC) 14x22 and the Ames Research Centers 40x80 low-speed wind tunnel facilities were conducted on a Boeing Hybrid Wing Body (HWB) configuration. These wind tunnel tests entailed various entries to evaluate the propulsion airframe interference effects including aerodynamic performance and aeroacoustics. In order to assist these tests in producing high quality data with minimal hardware interference, extensive Computational Fluid Dynamic (CFD) simulations were performed for everything from sting design and placement for both the wing body and powered ejector nacelle systems to the placement of aeroacoustic arrays to minimize its impact on the vehicles aerodynamics. This paper will provide a high level summary of the CFD simulations that NASA performed in support of the model integration hardware design as well as some simulation guideline development based on post-test aerodynamic data. In addition, the paper includes details on how multiple CFD codes (OVERFLOW, STAR-CCM+, USM3D, and FUN3D) were efficiently used to provide timely insight into the wind tunnel experimental setup and execution.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    NASA ERA Integrated CFD for Wind Tunnel Testing of Hybrid Wing-Body Configuration


    Contributors:
    J. A. Garcia (author) / J. E. Melton (author) / P. M. Stremel (author) / B. E. Nikaido (author) / R. E. Childs (author) / M. Schuh (author) / K. D. James (author) / K. R. Long (author) / D. D. Vicroy (author) / K. A. Deere (author)

    Publication date :

    2016


    Size :

    24 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    NASA ERA Integrated CFD for Wind Tunnel Testing of Hybrid Wing-Body Configuration

    Garcia, Joseph A. / Melton, John E. / Schuh, Michael et al. | NTRS | 2016


    NASA ERA Integrated CFD for Wind Tunnel Testing of Hybrid Wing-Body Configuration

    J. A. Garcia / J. E. Melton / P. M. Stremel et al. | NTIS | 2016


    NASA ERA Integrated CFD for Wind Tunnel Testing of Hybrid Wing-Body Configuration

    Garcia, Joseph A. / Melton, John E. / Schuh, Michael et al. | NTRS | 2016


    NASA ERA Integrated CFD for Wind Tunnel Testing of Hybrid Wing-Body Configuration (Invited)

    Garcia, Joseph A. / Melton, John / Schuh, Michael J. et al. | AIAA | 2016


    NASA ERA Integrated CFD for Wind Tunnel Testing of Hybrid Wing-Body Configuration (Invited) (AIAA 2016-0262)

    Garcia, Joseph A. / Melton, John / Schuh, Michael J. et al. | British Library Conference Proceedings | 2016