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Overall and blade- element performance of a 1.20-pressure-ratip fan stage at design blade setting angle [NASA TM X-3101 -- TM X-3110]

Series: National aeronautics and space administration. Publisher: WAShington, D. C. NASA 1974Description: 93p.

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Books	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	TM X-3101 (Browse shelf)	Available		TR2710

Total holds: 0

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Previous	TH668.9 ER82M MOBILITY OF POLYMER SOLUTIONS IN POROUS MEDIA	Thron, Wolfgang J. Topological structures	TM X 3232-3239 Nasa technical memorandum [TM X-3232--TM X-3239]	TM X-3101 Overall and blade- element performance of a 1.20-pressure-ratip fan stage at design blade setting angle [NASA TM X-3101 -- TM X-3110]	TN -1420 An application of lifting -surface theory to the prediction of angle-of -attack hinge - moment parameters for aspect ratio 4.5 wings [NASA TN D-1420 -- TN D-1429]	TN D-2491 Boundary layers on rotating spheres and other axisymmetric shapes.[NASA TN D-2491--TN D-2500]	TN D-411 Interim definitive orbit for the satellite 1959 alpha vanguard- II [NASA TN D-411--TN D-418]	Next

Bound with Nasa TM X-3101 to TM X-3110 [Accession Nos: TR2710 to TM X-2719]

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