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WIND-TUNNEL FLUTTER TESTS ON A DELTA WING WITH AN ALL-MOVING TIP CONTROL SURFACE.

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BookPublisher: Her Majesty'S Stationery Office, London 1956Description: 17.DDC classification: ARC | R&M 2978

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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 2978 (Browse shelf)	Not for loan		TR10798

Total holds: 0

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Previous	ARC R&M 2972 PRELIMINARY REPORT ON A GUST ALLEVIATOR INVESTIGATION ON A LANCASTER AIRCRAFT.	ARC R&M 2976 MODEL TESTING TECHNIQUE EMPLOYED IN THE R.A.E. SEAPLANE TANK.	ARC R&M 2977 THE REFLECTION EFFECT OF FENCES AT LOW SPEEDS.	ARC R&M 2978 WIND-TUNNEL FLUTTER TESTS ON A DELTA WING WITH AN ALL-MOVING TIP CONTROL SURFACE.	ARC R&M 3001 LOADING CONDITIONS OF TAILED AIRCRAFT IN LONGITUDINAL MANOEUVRES.	ARC R&M 3002 FLOW IN THE LAMINAR BOUNDARY LAYER NEAR SEPERATION.	ARC R&M 3004 THE INTERACTION BETWEEN SHOCK WAVES AND BOUNDARY LAYERS AT THE TRAILING EDGE OF A DOUBLE-WEDGE AEROFOIL AT SUPERSONIC SPEED.	Next

Bound With Arc R&M2960-77 Lack No.2961, 2973-75

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