A Two-Dimensional Bifurcated (2DB) Inlet was successfully tested in NASA Lewis Research Center s 10- by 10-Foot Supersonic Wind Tunnel. These tests were the culmination of a collaborative effort between the Boeing Company, General Electric, Pratt & Whitney, and Lewis. Extensive support in-house at Lewis contributed significantly to the progress and accomplishment of this test. The results, which met or exceeded many of the High-Speed Research (HSR) Program goals, were used to revise system studies within the HSR Program. The HSR Program is focused on developing low-noise, low-polluting, high-efficiency supersonic commercial aircraft. A supersonic inlet is an important component of an efficient, low-noise vehicle.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Two-Dimensional Bifurcated Inlet/Engine Tests Completed in 10- by 10-Foot Supersonic Wind Tunnel


    Contributors:


    Publication date :

    1999-04-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English






    Parametric Inlet Tested in Glenn's 10- by 10-Foot Supersonic Wind Tunnel

    Slater, John W. / Davis, David O. / Solano, Paul A. | NTRS | 2005


    WIND TUNNEL TESTS OF RECTANGULAR SUPERSONIC AIR INLET AT ITU

    Karpuzcu, Irmak Taylan / Yuceil, Kemal Bulent / Poyraz, Umit et al. | TIBKAT | 2019


    Parametric Inlet Tested in Glenn's 10- by 10-Foot Supersonic Wind Tunnel

    J. W. Slater / D. O. Davis / P. A. Solano | NTIS | 2005