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ANALYTICAL HEAT TRANSFER INVESTIGATION OF INSULATED LIQUID METHANE FUSELAGE TANKS FOR SUPERSONIC CRUISE AIRCRAFT.

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1971Description: 14.DDC classification: NASA | TN D-6157

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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-6157 (Browse shelf)	Not for loan		TR14542

Total holds: 0

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Previous	NASA TN D-6154 AXISYMMETRIC EXPANSION OF A PLASMA IN A MAGNETIC NOZZLE INCLUDING THERMAL CONDUCTION.	NASA TN D-6155 CALCULATED PRESSURE-INDUCED VIBRATIONAL ABSORPTION IN H2-H2 COLLISIONS IN HYDROGEN GAS.	NASA TN D-6156 FTIGUE LIVES AT 600 DEGHREE OF 120-MILLIMETER-BORE BALL BEARINGS OF AISI M-50,AISI M-1,AND WB-49 STEELS.	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	Next

Bound With Nasa Tn D-6151-6156,6158-6159.

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