Pressure signatures of F-100, F-104, and B-58 aircraft at distances from 120 to 425 ft from generating aircraft and at Mach numbers from 1.2 to 1.8 are shown; calculations made by using G.B.Whitham's method gave good agreement with experimental results; procedure for calculating F(y) function used relating to flow field is also given.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Experimental and calculated flow fields produced by airplanes flying at supersonic speeds


    Additional title:

    NASA -- Tech Note


    Contributors:
    Smith, H.J. (author)


    Publication date :

    1960


    Size :

    24 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




    MONITORING LOW-FLYING AIRPLANES

    HOHAUS LARS / KESSLER VINCENT / GERDES ALEXANDER | European Patent Office | 2018

    Free access

    Welding keeps airplanes flying

    Weymueller, C.R. | Tema Archive | 1978


    Airplanes for popular flying

    Klemin, A. | Engineering Index Backfile | 1938