Considerable research on large-scale high-performance, lift-engine, V/STOL configurations was conducted at Ames Research Center; exhaust gas reingestion characteristics, lift-engine inlet total-pressure recovery and distortion, and engine-airframe induced effects were measured in 40×80-ft wind tunnel both in and out of ground effects over wide range of transition flight conditions; results show that lift-engine configurations studied may have severe operational constraints placed upon them during transition. (06461)


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    Title :

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


    Additional title:

    SAE Paper


    Contributors:
    Barrack, J.P. (author) / Kirk, J.V. (author)

    Conference:

    SAE Meeting ; 1968 VTOL-STOL


    Published in:

    Publication date :

    1968


    Size :

    10 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :



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