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THERMAL FEASIBILITY OF USING METHANE OR HYDROGEN FUEL FOR DIRECT COOLING OF A FIRST-STAGE TURBINE STATOR

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BookPublisher: Nasa, Washington, D.C. 1970Description: 24.DDC classification: NASA | TN D-6042

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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-6042 (Browse shelf)	Not for loan		TR13639

Total holds: 0

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Previous	NASA TN D-6038 - COULOMB CORRECTIONS TO THE BETHE-HEITLER CROSS SECTIONS FOR ELECTRON-NUCLEUS BREMSSTRAHLUNG	NASA TN D-6039 - A DISCUSSION OF THE MODES OF FAILURE OF BUMPER-HULL STRUCTURES WITH APPLICATION TO THE METEOROID HAZARD	NASA TN D-6041 TESTS OF A FULL-SCALE ANNULAR RAM-INDUCTION COMBUSTOR FOR A MACH 3 CRUISE TURBOJET ENGINE	NASA TN D-6042 THERMAL FEASIBILITY OF USING METHANE OR HYDROGEN FUEL FOR DIRECT COOLING OF A FIRST-STAGE TURBINE STATOR	NASA TN D-6043 VELOCITY, INTERMITTENCY, AND TURBULENCE INTENSITY MEASUREMENTS IN THE BOUNDARY LAYER OF AN ACCELERATED FLOW	NASA TN D-6045 BURNING OF SOLID ALUMINUM AND MAGNESIUM SPHERES IN HIGH-TEMPERATURE AND HIGH-VELOCITY GASES	NASA TN D-6046 A PILOTED SIMULATOR INVESTIGATION OF GROUND EFFECT ON THE LANDING MANEUVER OF A LARGE, TAILLESS, DELTA-WING AIRPLANE	Next

Bound With Nasa Tn D-6040-41,6043-59

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