A 2.25% scale model of the space shuttle external tank and solid rocket boosters was tested in the NASA/Ames Unitary 11 x 11 foot transonic and 9 x 7 foot supersonic tunnels to obtain base pressure data with firing solid propellant exhaust plumes. Data system difficulties prevented the acquisition of any useful data in the 9 x 7 tunnel. However, 28 successful rocket test firings were made in the 11 x 11 tunnel, providing base pressure data at Mach numbers of 0.5, 0.9, 1.05, 1.2, and 1.3 and at plume pressure ratios ranging from 11 to 89.


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    Titel :

    Results of the NASA/Msfc FA-23 Plume Technology Test Program Performed in the NASA/Ames Unitary Wind Tunnels


    Beteiligte:

    Erscheinungsdatum :

    1977


    Format / Umfang :

    83 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    PIV IN NASA AMES UNITARY WIND TUNNELS

    Heineck, J. / Schairer, E. / Walker, S. et al. | British Library Conference Proceedings | 2011


    PIV in NASA Ames Unitary Wind Tunnels

    Heineck, James / Schairer, Edward / Walker, Stephen | AIAA | 2011