Various methods of engine testing and altitude facilities necessary for such research; selection of three basic types of altitude exhauster used at Lewis Flight Propulsion Laboratory, including reciprocating, rotary lobe, and centrifugal; limitations of each type and some of operational problems encountered; method of control and regulation.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Altitude test facilities for aircraft engine research


    Additional title:

    Chem Eng Progress


    Contributors:

    Published in:

    Publication date :

    1953


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Altitude Test apparatus for aircraft engine

    KIM EUN JONG / KIM DONG SIK / JEONG PIL JUN et al. | European Patent Office | 2018

    Free access


    PW4084 ENGINE TESTING IN ALTITUDE & SEA LEVEL TEST FACILITIES

    GLAZIER, JEFFREY R. / ROBERTS, JOHN H. / MASON, MARC W. et al. | SAE Technical Papers | 1994


    Rocket altitude test facilities register

    Ducasse, P. | TIBKAT | 1987


    Altitude and aircraft engine

    Pierce, E.F. | Engineering Index Backfile | 1940