After enumerating disadvantages connected with instruments using angle of incidence and impact pressure as impulse, author describes instrument working on principle of boundary layer thickness; reports on application during tunnel and flight tests. Report from German Research Institute, Berlin Adlershof.


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    Title :

    Simple determination of " Relation lift reserve" for airplane in vicinity of its minimum speed


    Additional title:

    Die eindeutige Kennzeichnung des Flugzustandes in der Naehe der Mindestgeschwindigkeit


    Contributors:
    Hoppe, F. (author)

    Published in:

    Publication date :

    1941


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German


    Keywords :


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