This report is a summary of a large number of research tasks performed in the area of low speed aerodynamics. The research projects are fundamental in nature but of relevance to the Navy. Both the theoretical and experimental aspects of each problem have been studied and the results are compared. Numerical methods have been used in self contained computer programs to calculate the aerodynamic performance of the following configurations: Two dimensional circulation controlled wings with blowing and regions of separated flow; two dimensional thrust augmented VTOL wings with jet entrainment effects; and rotors in hover with arbitrary twist, taper, and airfoil cross section using nonlinear lifting surface theory. Additional experimental work has been done in the area of rotor wake instabilities in and out of ground effect. (Modified author abstract)


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    Titel :

    Navy V/STOL Aerodynamics


    Beteiligte:
    J. B. Fanucci (Autor:in) / J. L. Loth (Autor:in) / N. Ness (Autor:in) / R. E. Walters (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    161 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    V/STOL aerodynamics

    Tema Archiv | 1975


    Aerodynamics of V/ STOL flight

    McCormick, Barnes W. | TIBKAT | 1967


    Aerodynamics of V/STOL aircraft

    Engineering Index Backfile | 1968


    Navy and V/STOL

    Weissman, C.C. | Engineering Index Backfile | 1962


    Some Aspects of STOL Aircraft Aerodynamics

    Loth, John L. | SAE Technical Papers | 1973