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ANALYSIS OF HELICOPTER MANEUVER-LOADS AND ROTOR-LOADS FLIGHT-TEST DATA

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BookPublisher: Nasa, Washington, D.C. 1973Description: 93.DDC classification: NASA | CR-2225

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA CR-2225 (Browse shelf)	Not for loan		TR12996

Total holds: 0

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Previous	NASA CR-2222 DEVELOPMENT OF PYRRONE STRUCTURAL FOAMS FOR HONEYCOMB FILLER	NASA CR-2223 SPECIFICATION OF MESOSPHERIC DENSITY, PRESSURE, AND TEMPERATURE BY EXTRAPOLATION	NASA CR-2224 DEVELOPMENT AND EVALUATION OF MAGNETIC AND ELECTRICAL MATERIALS CAPABLE OF OPERATING IN THE 800 DEGREE TO 1600 DEGREE F TEMPERATURE RANGE	NASA CR-2225 ANALYSIS OF HELICOPTER MANEUVER-LOADS AND ROTOR-LOADS FLIGHT-TEST DATA	NASA CR-2226 DEVELOPMENT OF A HIGH SPEED PARALLEL HYBRID BOOST BEARING	NASA CR-2228 AN IMPROVED METHOD FOR THE AERODYNAMIC ANALYSIS OF WING-BODY-TAIL CONFIGURATIONS IN SUBSONIC AND SUPERSONIC FLOW	NASA CR-2228 AN IMPROVED METHOD FOR THE AERODYNAMIC ANALYSIS OF WING-BODY-TAIL CONFIGURATIONS IN SUBSONIC AND SUPERSONIC FLOW	Next

Bound With Nasa Cr-2221-24,2226-29

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