Existing flight-test data on pitching angular accelerations have been compiled. The sources from which the data were taken were manufacturer's reports, NACA papers, and unpublished tests which were conducted at the Langley Aeronautical Laboratory. The compilation has been made for conventional airplanes that had moments of inertia which ranged from 535 to 572,000 slug- feet2. All the data available are for Mach numbers below 0.80.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Maximum Pitching Angular Accelerations of Airplanes Measured in Flight


    Beteiligte:
    C. E. Matheny (Autor:in)

    Erscheinungsdatum :

    1950


    Format / Umfang :

    20 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    Combined pitching and yawing motion of airplanes

    Von Baranoff, A. / Hopf, L. | Engineering Index Backfile | 1931


    Combined pitching and yawing motion of airplanes

    Baranoff, A. / Hopf, L. | TIBKAT | 1931


    Preliminary determination of normal accelerations of racing airplanes

    Scudder, N.F. / Kirschbaum, H.W. | Engineering Index Backfile | 1935