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EXPERIMENTAL PERFORMANCE AND COMBUSTION STABILITY OF A FULL-SCALE DUCT DURNER FOR A SUPERSONIC TURBOFAN ENGINE

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BookPublisher: Nasa, Washington, D.C. 1971Description: 82.DDC classification: NASA | TN D-6163

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-6163 (Browse shelf)	Not for loan		TR13030

Total holds: 0

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Previous	NASA TN D-616 - EXPERIMENTAL INVESTIGATION OF SOME OF THE PARAMETERS RELATED TO THE STABILITY AND CONTROL OF AERIAL VEHICLES SUPPORTED BY DUCTED FANS	NASA TN D-6161 COMPUTER PROGRAM FOR PRELIMINARY DESIGN AND ANALYSIS OF V/STOL TIP-TURBINE FANS	NASA TN D-6162 SOME CHARACTERISTICS OF A BOILING-WATER-COOLED VAPOR TRANSPORT FUEL PIN	NASA TN D-6163 EXPERIMENTAL PERFORMANCE AND COMBUSTION STABILITY OF A FULL-SCALE DUCT DURNER FOR A SUPERSONIC TURBOFAN ENGINE	NASA TN D-6164 DESIGN STUDY OF SHAFT FACE SEAL WITH SELF-ACTING LIFT AUGMENTATION	NASA TN D-6165 PRELIMINARY FRICTION AND WEAR STUDIES OF COBALT-RHENIUM SOLID SOLUTION ALLOY IN AIR AND IN VACUUM	NASA TN D-6166 FREQUENCY RESPONSE OF TWO TYPES OF LIQUID-METAL PRESSURE TRANSDUCERS WITH STANDOFF TUBES	Next

Bound With Nasa Tn D-6160-6162,6164-6169

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