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Effect of blade leading edge thickness on cavitation performance of 80.6 degree helical inducer in hydrogen [NASA TN D-5855]

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BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D.C. Nasa 1970Description: 21p.

Contents:

Technical Note D-5855

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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)		Not for loan		TR12738 [TN D-5855]

Total holds: 0

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Previous	Constrained chebyshev approximations to some elementary functions suitable for evaluation with floating point arithmetic [NASA TN D-6698]	Design, performance, and evaluation of a direct-current contactor for space nuclear electrical systems [NASA TN D-6699]	Observations of waterspouts and their parent clouds [NASA TN D-5854]	Effect of blade leading edge thickness on cavitation performance of 80.6 degree helical inducer in hydrogen [NASA TN D-5855]	Full-scale wind-tunnel investigation of the static longitudinal and lateral characteristics of a light single-engine low-wing airplane [NASA TN D-5857]	A 4-microsecond flashing light synchronized with framing of motion-picture cameras and its aplication in schlieren photography [NASA NT D-5858]	Report of Investegations 7651	Next

Bound With Nasa Tn D-5851-5854,5856-5860

Technical Note D-5855

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