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QUASI-ONE-DIMENSIONAL COMPRESSIBLE FLOW ACROSS FACE SEALS AND NARROW SLOTS.

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BookPublisher: Nasa, Washington, D.C. 1972Description: 37.DDC classification: NASA | TN D-6668

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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-6668 (Browse shelf)	Not for loan		TR15665

Total holds: 0

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Previous	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	NASA TN D-6672 PRACTICAL CONSIDERATIONS FOR ABEL INVERTING OF PHOTOGRAPHIC DATA WITH APPLICATION TO THE ANALYSIS OF A 15-KW WALL-STABILIZED ARC-LIGHT SOURCE	Next

Bound With Nasa Tn D-6660-6667,6669

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