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STRUCTURAL OPTIMIZATION OF SANDWICH AND RING-STIFFENED 120 DEGREE CONICAL SHELLS SUBJECTED TO EXTERNAL PRESSURE.

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BookPublisher: National Aeronautics And Space Administration, Washington, D.C. Description: 66.DDC classification: NASA | CR-1424

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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 CR-1424 (Browse shelf)	Not for loan		TR11387

Total holds: 0

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Previous	NASA CR-1420 EMISSIVITY COATINGS FOR LOW-TEMPERATURE SPACE RADIATORS	NASA CR-1422 LABORATORY OCULOMETER.	NASA CR-1423 EXPERIMENTAL INVESTIGATION IN AN ANNULAR CASCADE SECTOR OF HIGHLY LOADED TURBINE STATOR BLADING.	NASA CR-1424 STRUCTURAL OPTIMIZATION OF SANDWICH AND RING-STIFFENED 120 DEGREE CONICAL SHELLS SUBJECTED TO EXTERNAL PRESSURE.	NASA CR-1425 PROPERTIES OF NONAQUEOUS ELECTROLYTES.	NASA CR-1427 A FLIGHT INVESTIGATION OF SYSTEMS DEVELOPED FOR REDUCING PILOT WORKLOAD AND IMPROVING TRACKING ACCURACY DURING NOISE-ABATEMENT LANDING APPROACHES.	NASA CR-1428 GENERAL-AVIATION PILOT REACTIONS TO AND OPINIONS ON GROOVED RUNWAYS.	Next

Bound With Nasa Cr-1421-23, 1425

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