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HELICOPTER ROTOR BEHAVIOUR AFTER ENGINE FAILURE IN FORWARD FLIGHT :

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BookPublisher: HER MAJESTY'S STATIONERY OFFICE, LONDON 1955Description: ,13.Subject(s): REGIONAL PLANNING-ECONOMICASPECTS | LANDDDC classification: ARC R&M 2861

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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	ARC R&M 2861 (Browse shelf)	Not for loan		101871

Total holds: 0

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Previous	ARC R&M 2851 TUNNEL -WALL EFFECT ON AN AEROFOIL AT SUBSONIC SPEEDS	ARC R&M 2854 THE CRITICAL WHIRLING SPEEDS AND NATURAL VIBRATIONS OF A SHAFT CARRYING A SYMMETRICAL ROTOR	ARC R&M 2855 OSCILLATING WINGS IN COMPRESSIBLE SUBSONIC FLOW	ARC R&M 2861 HELICOPTER ROTOR BEHAVIOUR AFTER ENGINE FAILURE IN FORWARD FLIGHT	ARC R&M 2863 TESTS AT HIGH SUBSONIC SPEEDS ON A 10 PER CENT THICK PRESSURE-PLOTTING AEROFOIL OF RAE 104 SECTION	ARC R&M 2864 FORCE AND MOMENT MEASUREMENTS ON A CONICAL BODY AND A RECTANGULAR WING, SEPARATELY AND IN COMBINATION, AT MACH NUMBER 1.94	ARC R&M 2865 SOME APPLICATIONS OF THE LAM'E FUNCTION SOLUTIONS OF THE LINEARISED SUPERSONIC FLOW EQUATIONS	Next

Bound with ARC R&M 2862-2880.Lack No-2862,2868,2873

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