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THE AERODYNAMIC EFFECTS OF ASPECT RATIO AND SWEEPBACK ON WING FLUTTER.

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BookPublisher: Her Majesty'S Stationery Office, London 1957Description: 17.DDC classification: ARC | R&M 3011

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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 3011 (Browse shelf)	Not for loan Untraceable		TR11046

Total holds: 0

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Previous	ARC R&M 3008 VELOCITY DISTRIBUTION ON THIN TAPERED ARROWHEAD AND DELTA WINGS WITH SPANWISE CONSTANT THICKNESS RATIO AT ZERO INCIDENCE.	ARC R&M 3009 LOW-SPEED WIND-TUNNEL MEASUREMENTS OF LONGITUDINAL OSCILLATORY DERIVATIVES ON THREE WING PLAN-FORMS.	ARC R&M 3010 DERIVATIVE MEASUREMENTS AND FLUTTER TESTS ON A RECTANGULAR WING WITH A FULLL-SPAN CONTROL SURFACE, OSCILLATING IN MODES OF WING ROLL AND AILERON ROTATION.	ARC R&M 3011 THE AERODYNAMIC EFFECTS OF ASPECT RATIO AND SWEEPBACK ON WING FLUTTER.	ARC R&M 3012 SCALE EFFECTS AT HIGH SUBSONIC AND TRANSONIC SPEEDS, AND METHODS FOR FIXING BOUNDARY-LAYER TRANSITION IN MODEL EXPERIMENTS.	ARC R&M 3014 FLIGHT TESTS ON A VAMPIRE MK. 5 WITH A REDESIGNED ANTI-SNAKING RUDDER.	ARC R&M 3016 MEASUREMENTS OF THE PATHS OF THE VORTEX CORES SHED FROM THE WINGS OF A TYPICAL GUIDED-MISSILE MODEL AT M=I.57.	Next

Bound With Arc R&M 3000-3010, 3012-19 Lack No. 3003,13,15.

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