Considerable research on large-scale high-performance, lift-engine, V/STOL configurations has been conducted at Ames Research Center. The exhaust gas reingestion characteristics, lift-engine inlet total-pressure recovery and distortion, and engine-airframe induced effects were measured in the 40 × 80 ft wind tunnel both in and out of ground effect over a wide range of transition flight conditions. The results of these investigations show that the lift-engine configurations studied may have severe operational constraints placed upon them during transition.


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    Titel :

    Low-Speed Characteristics of High-Performance Lift-Engine V/STOL Aircraft


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    National Aeronautic and Space Engineering and Manufacturing Meeting ; 1968



    Erscheinungsdatum :

    01.02.1968




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





    Low-speed characteristics of high-performance lift-engine V/STOL aircraft

    Barrack, J.P. / Kirk, J.V. | Engineering Index Backfile | 1968


    High Lift Techniques for STOL Aircraft

    Cornish, J. J. / Tanner, R. F. | SAE Technical Papers | 1967



    Fan Lift-Cruise V/STOL Aircraft

    J. M. Peterson | NTIS | 1976