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    Aerodynamic Results of a Separation Test (CA20) Conducted at the Boeing Transonic Wind Tunnel Using 0.030-Scale Models of the Configuration 140A/B (Modified) Ssv Orbiter (Model No. 45-0) and the Boeing 747 Carrier (Model No. Ax 1319 I-1), Volume 2

    Aerodynamic Results of a Separation Test (CA20) Conducted at the Boeing Transonic Wind Tunnel Using 0.030-Scale Models of the Configuration 140A/B (Modified) Ssv Orbiter (Model No. 45-0) and the Boeing 747 Carrier (Model No. Ax 1319 I-1), Volume 2


    For abstract, see N76-16033.

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    Titel :

    Aerodynamic Results of a Separation Test (CA20) Conducted at the Boeing Transonic Wind Tunnel Using 0.030-Scale Models of the Configuration 140A/B (Modified) Ssv Orbiter (Model No. 45-0) and the Boeing 747 Carrier (Model No. Ax 1319 I-1), Volume 2

    Beteiligte:
    T. Dziubala (Autor:in) / V. Esparza (Autor:in) / R. L. Gillins (Autor:in) / M. Petrozzi (Autor:in)
    Erscheinungsdatum :

    1975

    Format / Umfang :

    1021 pages

    Medientyp :

    Report

    Format :

    Keine Angabe

    Sprache :

    Englisch

    Schlagwörter :

    Aerodynamics , Manned Spacecraft , Boeing 747 aircraft , Scale models , Space shuttle orbiters , Transonic wind tunnels , Wind tunnel tests , Aerodynamic characteristics , Angle of attack , Pressure distribution , Sideslip , Strain gages , Tables (Data)

    Ähnliche Titel

    Aerodynamic results of a separation test (CA20) conducted at the Boeing transonic wind tunnel using 0.030-scale models of the configuration 140A/B (modified) SSV orbiter (model no. 45-0) and the Boeing 747 carrier (model no. AX 1319 I-1), volume 1

    Dziubala, T. / Esparza, V. / Gillins, R. L. et al. | NTRS | 1975

    Aerodynamic results of a separation test (CA20) conducted at the Boeing transonic wind tunnel using 0.030-scale models of the configuration 140A/B (modified) SSV orbiter (model no. 45-0) and the Boeing 747 carrier (model no. AX 1319 I-1), volume 3

    Dziubala, T. / Esparza, V. / Gillins, R. L. et al. | NTRS | 1975

    Aerodynamic results of a separation test (CA20) conducted at the Boeing transonic wind tunnel using 0.030-scale models of the configuration 140A/B (modified) SSV orbiter (model no. 45-0) and the Boeing 747 carrier (model no. AX 1319 I-1), volume 2

    Dziubala, T. / Esparza, V. / Gillins, R. L. et al. | NTRS | 1975

    Aerodynamic Results of a Separation Test (CA20) Conducted at the Boeing Transonic Wind Tunnel Using 0.030-Scale Models of the Configuration 140A/B (Modified) Ssv Orbiter (Model No. 45-0) and the Boeing 747 Carrier (Model No. Ax 1319 I-1), Volume 3

    T. Dziubala / V. Esparza / R. L. Gillins et al. | NTIS | 1975

    Aerodynamic Results of a Separation Test (CA20) Conducted at the Boeing Transonic Wind Tunnel Using 0.030-Scale Models of the Configuration 140A/B (Modified) Ssv Orbiter (Model No. 45-0) and the Boeing 747 Carrier (Model No. Ax 1319 I-1), Volume 1

    T. Dziubala / V. Esparza / R. L. Gillins et al. | NTIS | 1975

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