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Development oaf an analysis for the determination of coupled helicopter rotor/control system dynamic response : Part 1 : analysis and applications [NASA CR - 2452]

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BookSeries: National Aeronautics and Space Administration [NASA]. Publisher: Washington, D.C. National Aeronautics and Space Administration [NASA] 1975Description: iii, 112p.DDC classification: NASA | CR - 2452

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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)	NASA CR - 2452 (Browse shelf)	Not for loan		TR007560

Total holds: 0

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Previous	NASA CR - 2449 Fluctuating surface-pressure characteristics on slender cones in subsonic, supersonic, and hypersonic mach-number flow	NASA CR - 2450 A wind model for an elevated stol-port configuration [NASA CR - 2450]	NASA CR - 2451 Development and application of a non-gaussian atmospheric turbulence model for use in flight simulation [NASA CR - 2451]	NASA CR - 2452 Development oaf an analysis for the determination of coupled helicopter rotor/control system dynamic response	NASA CR - 2453 Development oaf an analysis for the determination of coupled helicopter rotor/control system dynamic response	NASA CR - 2459 Investigation of land use of northern megalopolis using ERTS-1 imagery [NASA CR-2459 -- CR-2464]	NASA CR - 2522 Aerodynamic design and analysis system for supersonic aircraft [NASA CR-2522 -- CR-2525]	Next

Bound with NASA CR-2448-2453

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