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SPLITTING SUPERSONIC NOZZLE FLOW INTO SEPERATE JETS BY OVEREXPRESSION INTO A MULTILOBED DIVERGENT NOZZLE.

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BookPublisher: Nasa, Washington, D.C. 1972Description: 54.DDC classification: NASA | TN D-6667

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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-6667 (Browse shelf)	Not for loan		TR15664

Total holds: 0

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Previous	NASA TN D-6664 EXPERMENTAL INVESTIGATION OF THE FLOW,OXIDATION,COOLING, AND THERMAL-FATIGUE CHRACTERISTICS OF A LAMINATED POROUS SHEET MATERIAL.	NASA TN D-6665 MEASURED PERFORMANCE OF A 1089 K (1500 DEGREE F) HEAT SORAGE DEVICE FOR SUN-SHADE ORBITAL MISSIONS.	NASA TN D-6666 A METHOD FOR REDUCING GROUND REFELECTION EFFECTS FROM ACOUSTIC MEASUREMENTS.	NASA TN D-6667 SPLITTING SUPERSONIC NOZZLE FLOW INTO SEPERATE JETS BY OVEREXPRESSION INTO A MULTILOBED DIVERGENT NOZZLE.	NASA TN D-6668 QUASI-ONE-DIMENSIONAL COMPRESSIBLE FLOW ACROSS FACE SEALS AND NARROW SLOTS.	NASA TN D-6669 THE EFFECT OF INJECTION ANGLE ON THE INTERACTION BETWEEN SONIC SECONDARY JETS AND A SUPERSONIC FREE STREAM.	NASA TN D-6671 EVALUATION OF MASSLESS-SPRING MODELING OF SUSPENSION-LINE ELASTICITY DURING THE PARACHUTE UNFURLING PROCESS	Next

Bound With Nasa Tn D-6661-6666,6668-6669.

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