Experimental investigation of air-cooled turbine blades in turbojet engine V : rotor blades with split trailing edges

Authors
Publication date
Publisher

Abstract

Abstract is not available.

    Similar works

    Full text

    thumbnail-image

    Available Versions

    NASA Technical Reports Server

    redirect
    oaioai:casi.ntrs.nasa.gov:1993008...
    Last time updated on 03/08/2016