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EXPERIMENTAL EFFECTS OF GAS FLOW TRANSIENTS ON THE HEAT RELEASE OF BURNING LIQUID DROPS IN A ROCKET COMBUSTOR

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BookPublisher: Nasa, Washington, D.C. 1963Description: 19.DDC classification: NASA | TN D-1576 -

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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-1576 - (Browse shelf)	Not for loan		TR10077

Total holds: 0

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Previous	NASA TN D-1572 - EVALUATION OF DETAIL WIND DATA AS MEASURED BY THE EPS-16 RADAR/SPHERICAL BALLOON TECHNIQUE	NASA TN D-1573 - WIND FLOW IN THE 80-400 KM ALTITUDE REGION OF THE ATMOSPHERE	NASA TN D-1575 - TWO-DIMENSIONAL CRITICALITY CALCULATIONS OF GASEOUS-CORE CYLINDRICAL-CAVITYREACTORS	NASA TN D-1576 - EXPERIMENTAL EFFECTS OF GAS FLOW TRANSIENTS ON THE HEAT RELEASE OF BURNING LIQUID DROPS IN A ROCKET COMBUSTOR	NASA TN D-1577 - EFFECTS OF THE ACCELERATION DISTURBANCES ENCOUNTERED IN THE MA-7 SPACECRAFT ON THE LIQUID VAPOR INTERFACE IN A BAFFLED TANK DURING WEIGHTLESSNESS	NASA TN D-1578 - FEASIBILITY OF OPTIMIZING NOZZLE PERFORMANCE FOR ORBITAL-LAUNCH NUCLEAR ROCKETS	NASA TN D-1579 - PERFORMANCE CAPABILITY OF SINGLE-CAVITY VORTEX GASEOUS NUCLEAR ROCKETS	Next

Bound With Nasa Tn D-1571-90

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