• DocumentCode
    1370599
  • Title

    Altitude chamber requirements for evaluating blast-cooled aircraft generators

  • Author

    Scott, H. Dale

  • Author_Institution
    Naval Research Laboratory, Washington, D. C.
  • Volume
    71
  • Issue
    6
  • fYear
    1953
  • Firstpage
    427
  • Lastpage
    430
  • Abstract
    ALTITUDE chambers have proved beneficial in the development of equipment to be installed in aircraft. By determining the conditions under which the equipment is to be operated and then simulating those conditions in altitude chambers, it has been possible to discover deficiencies and make corrections prior to installation of the equipment in aircraft. This procedure has made it possible to complete the development programs on the auxiliary equipment so that flight-test emphasis has been on the overall performance of the aircraft. Aircraft performance has been aided materially by the use of altitude chambers.
  • Keywords
    Aircraft; Aircraft propulsion; Cooling; Equations; Generators; Heating; Shafts;
  • fLanguage
    English
  • Journal_Title
    American Institute of Electrical Engineers, Part II: Applications and Industry, Transactions of the
  • Publisher
    ieee
  • ISSN
    0097-2185
  • Type

    jour

  • DOI
    10.1109/TAI.1953.6371313
  • Filename
    6371313