Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Design of Mach 2.4 Quiet Nozzles for the NASA Langley Supersonic Low-Disturbance Pilot Tunnel


    Contributors:

    Conference:

    18th Aerospace ground testing conference ; 1994 ; Colorado Springs; CO



    Publication date :

    1994-01-01


    Size :

    ALL


    Remarks:

    Papers AIAA-94-2500 - 2699 with gaps held only


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    NASA Langley Mach 6 Quiet Wind-Tunnel Performance

    Alan E. Blanchard / Jason T. Lachowicz / Stephen P. Wilkinson | AIAA | 1997


    Supersonic and hypersonic quiet tunnel technology at NASA Langley

    WILKINSON, S. / ANDERS, S. / CHEN, F.-J. et al. | AIAA | 1992


    Performance of the NASA-Langley Mach 6 Quiet Wind Tunnel

    Blanchard, Alan / Lachowicz, Jason / Wilkinson, Stephen | AIAA | 1996


    Design requirements for the NASA Langley supersonic low-disturbance wind tunnel

    BECKWITH, I. / CHEN, F.-J. / CREEL, JR., T. | AIAA | 1986