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VIBRATION AND FLUTTER TESTS OF A PRESSURIZED THIN-WALLED TRUNCATED CONICAL SHELL

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BookPublisher: Nasa, Washington, D.C. 1971Description: 24.DDC classification: NASA | TN D-6106

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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-6106 (Browse shelf)	Not for loan		TR12502

Total holds: 0

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Previous	NASA TN D-6103 FLOW FIELD RESULTING FROM FORWARD-FACING NOZZLES EXHAUSTING NEAR A LARGE CYLINDRICAL BODY AT FREE-STREAM MACH NUMBERS OF 3.0, 4.5, AND 6.0	NASA TN D-6104 AN APPROACH TO THE DETERMINATION OF AIRCRAFT HANDLING QUALITIES BY USING PILOT TRANSFER FUNCTIONS	NASA TN D-6105 INVESTIGATION OF FLAMELESS COMBUSTION MECHANISM OF M-2 DOUBLE-BASE PROPELLANT	NASA TN D-6106 VIBRATION AND FLUTTER TESTS OF A PRESSURIZED THIN-WALLED TRUNCATED CONICAL SHELL	NASA TN D-6107 AN EVALUATION OF THE SLURRY COMPACTION PROCESS FOR THE FABRICATION OF METAL-MATRIX COMPOSITES	NASA TN D-6108 FLIGHT INVESTIGATION OF VTOL CONTROL AND DISPLAY CONCEPT FOR PERFORMING DECELERATING APPROACHES TO AN INSTRUMENT HOVER	NASA TN D-6109 ACCURACY OF ESTIMATING THE LOCATION OF A LANDED SPACECRAFT ON MARS FROM RANGE AND RANGE-RATE DATA	Next

Bound With Nasa Tn D-6100-6105,6107-6109

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