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EFFECT OF INJECTION ELEMENT RADIAL DISTRIBUTION AND CHAMBER GEOMETRY ON ACOUSTIC-MODE INSTABILITY IN A HYDROGEN OXYGEN ROCKET

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BookPublisher: Nasa, Washington, D.C. 1969Description: 43.DDC classification: NASA | TN D-5375 -

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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-5375 - (Browse shelf)	Not for loan		TR9339

Total holds: 0

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Previous	NASA TN D-5372 - STABILITY OF TWO-FLUID WHEEL FLOWS WITH AN IMPOSED UNIFORM AXIAL MAGNETIC FIELD	NASA TN D-5373 - COMPUTER PROGRAM FOR VISCOUS, ISOTHERMAL COMPRESSIBLE FLOW ACROSS A SEALING DAM WITH SMALL TILT ANGLE	NASA TN D-5374 - CAUSES, MEASUREMENT, AND ELIMINATION OF FUEL-ELEMENT FISSION PRODUCT LEAKAGE AT THE NASA PLUM BROOK REACTOR	NASA TN D-5375 - EFFECT OF INJECTION ELEMENT RADIAL DISTRIBUTION AND CHAMBER GEOMETRY ON ACOUSTIC-MODE INSTABILITY IN A HYDROGEN OXYGEN ROCKET	NASA TN D-5376 - OXIDATION AND THERMAL FATIGUE CRACKING OF NICKEL-AND COBALT-BASE ALLOYS IN A HIGH VELOCITY GAS STREAM	NASA TN D-5377 - EXPERIMENTAL AND THEORETICAL TURBULENT BOUNDARY LAYER DEVELOPMENTIN A MACH 4.4 WATER-COOLED CONICAL NOZZLE	NASA TN D-5378 - AERODYNAMIC CHARACTERISTICS IN PITCH OF A 1/7-SCALE MODEL OF A TWO- AND THREE-STAGE ROCKET CONFIGURATION AT MACH NUMBERS OF 0.4 TO 4.63	Next

Bound With Nasa Tn D-5371-80

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