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Experimental performance and combustion stabilty of a full scale duct burner for a supersonic turbofan engine [NASA TN D-6163]tburner for a supersonic turbofan engine [NASA TN D-6161]

By: Contributor(s): Material type: TextTextLanguage: English Publication details: Washingtion, D. C. NASA March 1971Description: 82p
Contents:
NASA technical note
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Holdings
Item type Current library Collection Call number Status Date due Barcode Item holds
Technical Report Technical Report PK Kelkar Library, IIT Kanpur Reference Not for loan TR013030
Total holds: 0

NASA technical note

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