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EXPERIMENTAL INVESTIGATION OF COAXIAL JET MIXING OF TWO SUBSONIC STREAMS AT VARIOUS TEMPERATURE, MACH NUMBER, AND DIAMETER RATIOS FOR THREE CONFIGURATIONS

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BookPublisher: Nasa, Washington, D.C. 1959Description: 29.DDC classification: NASA | MEMO 12-21-58E

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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 MEMO 12-21-58E (Browse shelf)	Not for loan Untraceable		TR14066

Total holds: 0

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Previous	NASA MEMO 12-15-58L - FREE-FLIGHT INVESTIGATION OF A ROCKET-PROPELLED MODEL TO DETERMINE THE AERODYNAMIC HEATING ON A THIN, UNSWEPT, UNTAPERED, MULTISPAR, ALUMINUM -ALLOY WING AT MACH NUMBERS UP TO 2.22	NASA MEMO 1-21-59A - EXPERIMENTAL INVESTIGATION OF THE PRESSURE RISE REQUIRED FOR INCIPIENT SEPARATION OF TURBULENT BOUNDARY LAYERS IN TWO-DIMENSIONAL SUPERSONIC FLOW	NASA MEMO 12-20-58L - INVESTIGATION OF THE MAXIMUM SPIN-UP COEFFICIENT OF FRICTION OBTAINED DURING TESTS OF A LANDING GEAR HAVING A STATIC-LOAD RATING OF 20,000 POUNDS	NASA MEMO 12-21-58E EXPERIMENTAL INVESTIGATION OF COAXIAL JET MIXING OF TWO SUBSONIC STREAMS AT VARIOUS TEMPERATURE, MACH NUMBER, AND DIAMETER RATIOS FOR THREE CONFIGURATIONS	NASA MEMO 12-21-58L - TOTAL-PRESSURE RECOVERY AND DRAG CHARACTERISTICS OF SEVERAL AUXILIARY INLETS AT TRANSONIC SPEEDS	NASA MEMO 12-22-58E PERFORMANCE OF A MACH NUMBER 3.0 DESIGN AXISYMMETRIC DOUBLE-CONE EXTERNAL-COMPRESSION INLET IN MACH NUMBER RANGE 2.07 TO 1.48	NASA MEMO 12-23-58E A STUDY OF OXIDATION OF HYDROGEN BASED ON FLASHBACK OF HYDROGEN-OXYGEN-NITROGEN BURNER FLAMES	Next

Bound With Nasa Memo 12-8-58e-12-13-58e, 12-22-58e-12-29-58e Lack No. 12-9-58e, 12-12-58e, 12-14-58e-12-20-58e, 12-25-58e-12-28-58e.

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