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COMPUTER PROGRAM FOR PRELIMINARY DESIGN AND ANALYSIS OF V/STOL TIP-TURBINE FANS

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BookPublisher: Nasa, Washington, D.C. 1971Description: 141.DDC classification: NASA | TN D-6161

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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-6161 (Browse shelf)	Not for loan		TR13028

Total holds: 0

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Previous	NASA TN D-6157 ANALYTICAL HEAT TRANSFER INVESTIGATION OF INSULATED LIQUID METHANE FUSELAGE TANKS FOR SUPERSONIC CRUISE AIRCRAFT.	NASA TN D-6159 HYDRODYNAMIC ENTRANCE EFFECT ON BOILING HAD NEAR CRIRICAL HYDROGEN HEAT TRANSFER.	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	Next

Bound With Nasa Tn D-6160,6161-6169

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