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THEORICAL BUCKLING LOADS OF BORON/ALUMINUM AND GRAPHITE/RESIN FIBER-COMPOSITE ANISOTROPIB

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1971Description: 36.DDC classification: NASA | TN D-6572

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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-6572 (Browse shelf)	Not for loan		TR15523

Total holds: 0

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Previous	NASA TN D-650 SOME EFFECTS OF NOSE BLUNTNESS AND FINENESS RATIO ON THE STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF BODIES OF REVOLUTION AT SUBSONIC SPEEDS	NASA TN D-6523 - EXPERIMENTAL INVESTIGATION OF LAMINAR GAS JET DIFFUSION FLAMES IN ZERO GRAVITY	NASA TN D-6529 - THIN -SHOCK-LAYER SOLUTION FOR NONEQUILIBRIUM INVISCID HYPERSONIC FLOWS IN EARTH,MARTIAN,AND VENUSIAN ATMOSPHERES	NASA TN D-6572 THEORICAL BUCKLING LOADS OF BORON/ALUMINUM AND GRAPHITE/RESIN FIBER-COMPOSITE ANISOTROPIB	NASA TN D-6574 EXPERIMENTAL BOUNDARY-LAYER EDGE MACH NUMBERS FOR TWO SPACE SHUTTLE ORBITERS AT HYPERSONIC SPEEDS.	NASA TN D-6575 SUMMARY OF SPIN TECHNOLOGY AS RELATED TO LIGHT GENERAL-AVIATION AIRPLANES.	NASA TN D-6576 ROTATIONAL-TEMPERATURE DETERMINATION IN FLOWING NITROGEN USING AN ELECTRON BEAM.	Next

Bound With Nasa Tn D-6571,6573-6578lack No.6573,6577.

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