Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1952


    Size :

    53 pages


    Remarks:

    Illus, Diagrs, Charts, Tables


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English





    Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities

    Chapman, Dean R / Wimbrow, William R / Kester, Robert H | NTRS | 1952


    Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities

    Chapman, D.R. / Winbrow, W.R. / Kester, R.H. | Engineering Index Backfile | 1952


    Blunt Trailing Edge Cooling Effects at Supersonic Regime

    Saracoglu, Bayindir / Paniagua, Guillermo / Rambaud, Patrick | AIAA | 2009