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OSCILLATORY-DERIVATIVE MEASUREMENTS ON STINGMOUNTED WING-TUNNEL MODELS : METHOD OF TEST AND RESILTS FOR PITCH AND YAW ON A CAMBERED OGEE WING AT MACH NUMBERS UP TO 2.6

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BookPublisher: Her Majesty'S Stationery Office, London 1964Description: 52.DDC classification: ARC | R&M 3355

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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 3355 (Browse shelf)	Not for loan Untraceable		TR11186

Total holds: 0

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Previous	ARC R&M 3351 THE USE OF SURFACE PITOT TUBES AS SKIN-FRICTION METERS AT SUPERSONIC SPEEDS.	ARC R&M 3352 A NOTE ON THE THEORY OF PARACHUTE STABILITY.	ARC R&M 3354 THE ESTIMATION OF STRESSES AROUND UNREINFORCED HOLES IN INFINITE ELASTIC SHEETS.	ARC R&M 3355 OSCILLATORY-DERIVATIVE MEASUREMENTS ON STINGMOUNTED WING-TUNNEL MODELS	ARC R&M 3356 A THEORETICAL ANALYSIS OF THE STABILITY OF AN AEROPLANE ON NORTHERLY HEADINGS WHEN CONTROLLED BY AN AILERON-STEERING AUTOPILOT MONITORED FROM A GYRO-MAGNETIC COMPASS.	ARC R&M 3382 AN EXPERIMENT ON AERODYNAMIC NOZZLES AT M=2.	ARC R&M 3383 ON LIFTING BODIES WHICH CONTAIN TWO-DIMENSIONAL SUPERSONIC FLOWS.	Next

Bound Wiyh:Arc R&M 3341-3354,3356-3360.Lack No.Arc R&M 3343,45,49,50,53,59

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