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AM IMPROVED METHOD FOR CALCULATING GENERALISED AIRFORCES ON OSCILLATING WINGS IN SUBSONIC FLOW

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BookPublisher: Her Majesty'S Stationery Office,London 1971Description: 17.DDC classification: ARC | R&M 3657

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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 3657 (Browse shelf)	Not for loan		TR17143

Total holds: 0

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Previous	ARC R&M 3654 STRENGTH VARIABLITY IN STRUCTURAL MATERIALS	ARC R&M 3655 LOW-SPEED WIND-TUNNEL TESTS ON A SWEPTBACK WING MODEL(BUCCANEAER MARK 1) WITH BLOWING AT THE WING LEADING EDGE AND BLOWING OVER THE FLAPS AND DROOPED ATLERONS	ARC R&M 3656 ON THE STATIC PERFORMANCE OF TWO-DIMENSIONAL INTAKES WITH MOMENTUM INJECTION IN THE FORM OF BOUNDARY-LAYER CONTROL BY BLOWING	ARC R&M 3657 AM IMPROVED METHOD FOR CALCULATING GENERALISED AIRFORCES ON OSCILLATING WINGS IN SUBSONIC FLOW	ARC R&M 3658 A METHOD OF CORRELATING THE GROUND EFFECTS ON THE LONGITUINAL CHARACTERISIECS OF SLENDER WINGS	ARC R&M 3659 SONIC BANG MEASUREMENTS DURING EXERCISE SUMMER SKY	ARC R&M 3661 MEASUREMENTS OF SECTION PRESSURE DISTRIBUTION AT A MACH NUMBER OF 2.0 ON A WING OF 70 DEGREES SWEEP MOUNTED ON A WAISTED BODY	Next

Bound With Arc R&M-3650-3656,3658-3659.

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