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  • AIRCRAFT PROPULSION AND POWER  (1)
  • 1975-1979  (1)
  • 1920-1924
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  • 1
    Publication Date: 2019-06-27
    Description: Tests were conducted to determine if there are performance penalties associated with the installation of infrared (IR) suppressors on the T63-A-700 turboshaft engine. The testing was done in a sea-level, static test cell. The same engine (A-E402808 B) was run with the standard OH-58 aircraft exhaust stacks and with the ejector-type IR suppressors in order to make a valid comparison. Repeatability of the test results for the two configurations was verified by rerunning the conditions over a period of days. Test results showed no measurable difference in performance between the standard exhaust stacks and the IR suppressors.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: NASA-TM-78970 , E-9730 , AVRADCOM-TR-78-38(PL)
    Format: application/pdf
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