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NASA Technical Note [NASA TN D-382]: Effect of blade cutout on power required by helicopters operating at high tip-speed ratios

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Material type: Text

TextLanguage: English Series: National Aeronautics and Space Administration | NASA Technical NotePublication details: NASA 1960 WashingtonDescription: 18pSubject(s):

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Holdings
Item type	Current library	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D-381 to 390	Not for loan		TR15585

Total holds: 0

Previous	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	Next
Previous	Relationship between magnitude of applied spin recovery moment and ensuing of recovery turns [NASA TN D-4077]	An evaluation of sea surface temperature as measured by the nimbus I high resolution infrared radiometer [NASA TN D-4078]	Hypersonic aerodynamics charectristics of minimum wave drag bodies having variations in cross sectional shape [NASA TN D-4079]	NASA Technical Note [NASA TN D-382]: Effect of blade cutout on power required by helicopters operating at high tip-speed ratios	NASA Technical Note [NASA TN D-383]: Theoretical calculations of the pressures forces, and moments due to various lateral motions acting on tapered sweptback vertical tails with supersonic leading and trailing edges	NASA Technical Note [NASA TN D-384]: Combinations of shear, compressive thermal, and compressive load stresses for the onset of permanent buckles in plates	NASA Technical Note [NASA TN D-386]: Statistical data on control motions and airplane response of a republic F-84F airplane during operational training missions	Next

Bound together NASA TN D-381 to 390

Bound vol. Acc. No. 63662 contains Acc. No. TR15585 to TR15589, TR15610, TR15590 to TR15591 & TR15611

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