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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]

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Material type: Text

TextLanguage: English Publication details: Washingtion, D. C. NASA March 1971Description: 82p

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NASA technical note

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Holdings
Item type	Current library	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	Reference		Not for loan		TR013030

Total holds: 0

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Previous	Wear and friction of impregnated mechanical carbons at temperatuures to 1400 degree F (760 degree C) in air or nitrogen [NASA TN D-3958	Computer program for preliminary design and analysis of V/STOL tip turbine fans [NASA TN D-6161]	Some characteristics of a boiling water cooled vapor transport fuel pin [NASA TN D-6162]]	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]	An study of shaft face sear self acting lift augmentatuio [NASA TN D-6164]	Preliminary friction and wear studies ogf cobalt rehenium solid solution alloy in air and in vaccum [NASA TN D-6165]	Performance of a short modular turbojet combustor segment using ASTM-A1 fuel [NASA TN D-6167]	Next

NASA technical note

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