CORRECTION of night test climb data to account for departure of the variables from standard or specified conditions presents a major problem owing to the large number of parameters involved. Atmospheric conditions invariably depart from standard I.C.A.N., and seldom do values of aircraft weight, speed and r.p.m. agree with those specified in a theoretical consideration of the problem. This article describes a method used to analyse climb data whereby climb performance of an aircraft may be established for specified conditions, speed for best rate of climb determined and comparison made with theoretical estimates. Rigid flying procedure is not required, and flying time is reduced to a minimum.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    The Rate of Climb of Turbo-Jet Aircraft


    Subtitle :

    A Method of Analysing Test Data to Establish the Climb Performance of an Aircraft


    Contributors:


    Publication date :

    1952-02-01


    Size :

    3 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Rate of climb of turbo-jet aircraft

    Whittley, D.C. | Engineering Index Backfile | 1952


    The turbo fan aircraft minimum cost climb technique

    Mirosavljević, P. / Gvozdenović, S. / Čokorilo, O. | Emerald Group Publishing | 2009


    The turbo fan aircraft minimum cost climb technique

    Mirosavljevic, P. | Online Contents | 2009


    Aircraft rate-of-climb indicators

    Johnson, D.P. | Engineering Index Backfile | 1939


    Aircraft rate-of-climb indicators

    Johnson, Daniel P. | TIBKAT | 1939