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Note on helicopter rotor-blade fatigue-crack propagation rates under equivalent-lifetime fatigue loadings[NASA TN D -1018]

By: Ward,John F.

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BookSeries: National Aeronautics and Space Adminstration ; NASA technical note. Publisher: Washington, D.C. National Aeronautics and Space Adminstration 1962Description: 10p.Subject(s): Helicopter rotor-blade

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Item type	Current location	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D 1011-1020	Not for loan		TR10375

Total holds: 0

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Previous	Theoretical evaluation of hypersonic forces, moments, and stability derivatives for a combination of flat plates, including effects of blunt leading edges by Newtonian impact theory[NASA TN D-1015]	Jet effects on cylindrical afterbodies housing sonic and supersonic nozzles which exhaust against a supersonic stream at angles of attack from 90 degree to 180 degree [NASA TN D-1016]	Exploratory investigation of jet-blast effects on a dust-covered surface at low ambient pressure[NASA TN D -1017]	Note on helicopter rotor-blade fatigue-crack propagation rates under equivalent-lifetime fatigue loadings[NASA TN D -1018]	Geomagnetic- and interplanetary-magnetic-field environment of an earth satellite [NASA TN D-1019]	Further developments on the required number of randomly spaced communication and navigation satellites[NASA TN D -1020]	NASA TM [X-72]	Next

Bound vol. contains D 1011-1020

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