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EXPERIMENTAL INVESTIGATION OF THE EFFECT OF ENGINE LOADS ON WING STRUCTURES

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BookPublisher: Her Majesty'S Stationery Office,London 1957Description: 15.DDC classification: HMSO-R&M-3062 | -

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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	HMSO-R&M-3062 - (Browse shelf)	Not for loan		TR8905

Total holds: 0

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Previous	HMSO-R&M-3059 - CALCULATION OF DERIVATIVES FOR A CROPPED DELTA WING WITH AN OSCILLATING CONSTANT-CHORD FLAP IN A SUPERSONIC AIR STREAM	HMSO-R&M-3060 - CALCULATION OF DERIVATIVES FOR A CROPPED DELTA WING WITH SUBSONIC LEADING EDGES OSCILLATING IN A SUPERSONIC AIR STREAM	HMSO-R&M-3061 - NOTE ON THE CONVERGENCE OF NUMERICAL SOULITIONS OF THE NAVIER-STROKES EQUATIONS	HMSO-R&M-3062 - EXPERIMENTAL INVESTIGATION OF THE EFFECT OF ENGINE LOADS ON WING STRUCTURES	HMSO-R&M-3063 - SAMPLING ERRORS OF ATMOSPHERICTURBULENCE MEASUREMENTS	HMSO-R&M-3064 - EXPERIMENTS ON TWO-DIMENSIONAL BASE FLOW AT M = 2.4	HMSO-R&M-3065 - EFFECT OF WING-TAILPLANE AERODYNAMIC INTERACTION ON TAIL FLUTTER	Next

Bound With Hmso-R&M-3050-69

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