This paper presents an overview of supporting technology programs conducted to reduce the risk in the joint NASA/Navy Lift/Cruise Fan Research and Technology Aircraft Program. The aeronautical community has endeavored to combine the low-speed and lifting capabilities of the helicopter with the high-speed capabilities of the jet aircraft; recent developments have indicated a lift/cruise fan propulsion system may provide these desired characteristics. NASA and the Navy have formulated a program that will provide a research and technology aircraft to furnish viability of the lift/cruise fan aircraft through flight experiences and obtain data on designs for future naval and civil V/STOL aircraft. The supporting technology programs discussed include: (1) design studies for operational aircraft, a research and technology aircraft, and associated propulsion systems; (2) wind-tunnel tests of several configurations; (3) propulsion-system thrust vectoring tests; and (4) simulation. These supporting technology programs have indicated that a satisfactory research and technology aircraft program can be accomplished within the current level of technology.


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    Titel :

    Review of V/STOL lift/cruise fan technology


    Beteiligte:
    Rolls, L. S. (Autor:in) / Quigley, H. C. (Autor:in) / Perkins, R. G., Jr. (Autor:in)

    Kongress:

    Aircraft Systems and Technology Meeting


    Erscheinungsdatum :

    1976-09-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Review of V/STOL lift/cruise fan technology

    ROLLS, L. / QUIGLEY, H. / PERKINS, JR., R. | AIAA | 1976


    Fan Lift-Cruise V/STOL Aircraft

    J. M. Peterson | NTIS | 1976