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ANALYTICAL AND EXPERIMENTAL INVESTIGATION OF AIRCRAFT METAL STRUCTURES REINFORCED WITH FILAMENTARY COMPOSITES

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BookPublisher: Nasa, Washington, D.C. 1973Description: VII,105.DDC classification: NASA | CR-2122 -

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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-2122 - (Browse shelf)	Not for loan		TR7973

Total holds: 0

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Previous	NASA CR-2118 JIMSPHERE WIND AND TURBULANCE EXCEEDANCE STATISTICS	NASA CR-2119 DIFFERETIAL CORRECTION SCHEMES IN NONLINEAR REGRESSION	NASA CR-2120 SUMMARY OF NONDESTRUCTIVE TESTING THEORY AND PRACTICE	NASA CR-2122 - ANALYTICAL AND EXPERIMENTAL INVESTIGATION OF AIRCRAFT METAL STRUCTURES REINFORCED WITH FILAMENTARY COMPOSITES	NASA CR-2123 - ASYMMETRIC HYPERSONIC FLOW	NASA CR-2124 - A FINITE-DIFFERENCE METHOD FOR PREDICTING SUPERSONIC TURBULENT BOUNDARY-LAYER FLOW WITH TANGENTIAL SLOT INJECTION	NASA CR-2125 - THERMAL DYNAMIC MODELING STUDY	Next

Bound With Nasa Cr-2121-29

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