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BAFFLE THICKNESS EFFCTS IN FUEL SLOSHING EXPRERIMNTS.

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BookPublisher: Nasa, Washington, D.C. 1966Description: 12.DDC classification: NASA | TN D-3716

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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-3716 (Browse shelf)	Not for loan Untraceable		TR15625

Total holds: 0

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Previous	NASA TN D-3712 USE OF ANLOG COMPUTATION IN PERDICATING DYNAMIC TEMERATURE EXCURSIONS OF ORBITING SPACECRAFT.	NASA TN D-3713 THE EFFECTIVENESS OF SYSTEMS TESTS IN ATTAINING RELIABLE EARTH SATELLITE PERFORMANCE.	NASA TN D-3714 A STUDY OF EMBEDMENT AND OTHER MATALLURGICAL AND MECHNICAL CHARACTERISTICS OF CROSS-WIRE RESSISTENCE WELDS.	NASA TN D-3716 BAFFLE THICKNESS EFFCTS IN FUEL SLOSHING EXPRERIMNTS.	NASA TN D-3717 THE NEAR-EARTH METEROID ENVIORNMENT	NASA TN D-3718 SUBSONIC LONGITUDINAL AERODYNAMIC CHRACTERISTICS OF A 40 DEGREE SEMIAPEX ANGLE CONICAL REENTRY CONFIGURATION.	NASA TN D-3719 EXPERIMENTAL PERFORMANCE OF A CONTROL PRESSURE PROBE AT MACH NUMBERS OF 3.0,4.5, AND 6.0.	Next

Bound Withg Nasa Tn D-3712-3715,3717-3720.

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