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Simlified method of determining the elastic state of thermal stress in a thin, flate plate of finite dimensions

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BookPublisher: Wasighnton D. C. Nasa Aeronautics And Space Administration [NASA] 1963Description: 23p.Subject(s): Thermodynamics and CombustionDDC classification: NASA | TN D-1740 Summary:

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA TN D-1740 (Browse shelf)	Not for loan		TR18436

Total holds: 0

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Previous	NASA TN D-1737 A General IBM 704 or 7090 computer program for computation of chemical equilibrium compositions, rocket performance and chapman-jouguet detonations	NASA TN D-1738 Effects of regenrative and radiation cooling on performance of electrothermal thrustors	NASA TN D-1739 Compatibility of cesium vapor with selected materials at temperatures to 1200 celsius F	NASA TN D-1740 Simlified method of determining the elastic state of thermal stress in a thin, flate plate of finite dimensions	NASA TN D-1801 Maneuver accelerations experienced during routine operations of a commercial turbojet transport airplane [NASA TN D - 1801--TN D-1810]	NASA TN D-1802 FLIGHT OPERATING PROBLEMS AND AERODYNAMIC AND PERFORMANCE CHRACTERISTICS OF A FIXED-WING, TILT-DUCT,VTOL RESEARCH AIRCRAFT.	NASA TN D-1806 INVESTIGATION OF PROPELLER-POWER-PLANT AUTOPRECESSION BOUNDARIES FOR A DYNAMIC-AEROELASTIC MODEL OF A FOUR ENGINE TURBOPROP TRANSPORT AIRPLANE.	Next

Bound With the NASA TN D-1731-1739

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