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CALIBRATION OF THE R.A.E BEDFORD 8FT.WIND TUNNEL AT SUBSONIC SPEEDS,INCLUDING A DISCUSSION OF THE CORRECTIONS APPLIED TO THE MEASURED PRESSURE DISTRIBUTION TO THE CALIBRATION DIRECT AND BLOCKAGE EFFEC

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BookPublisher: Her Majesty'S Stationery Office, London 1969Description: 58.DDC classification: ARC | R&M 3583

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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 3583 (Browse shelf)	Not for loan		TR17054

Total holds: 0

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Previous	ARC R&M 3578 SOME INVESTIGATIONS INTO THE SPANWISE NON-UNIFORMITY OF NOMINALLY TWO-DIMENSIONAL INCOM-PRESSIBLE BOUNDARY LAYERS DOWNSTREAM OF GAUZE SCREENS	ARC R&M 3579 CALCULATIONS SHOWING THE INFLUENCE OF AERODYNAMIC DAMPING ON BINARY WING FLUTTER	ARC R&M 3581 Co-ordinated experimental and theoretical research on the Oscillatory airforces for selected plamforms at subsonic and supersonic speeds.	ARC R&M 3583 CALIBRATION OF THE R.A.E BEDFORD 8FT.WIND TUNNEL AT SUBSONIC SPEEDS,INCLUDING A DISCUSSION OF THE CORRECTIONS APPLIED TO THE MEASURED PRESSURE DISTRIBUTION TO THE CALIBRATION DIRECT AND BLOCKAGE EFFEC	ARC R&M 3584 VARIBLE STABILITY AND CONTROL TESTS ON THE S.C.I AIRCRAFT IN JET-BORNE FLIGHT, WITH PARTICULAR REFERENCE TO DESIRABLE VTOL FLYING QUALITIES	ARC R&M 3585 THE PERFORMANCE OF SOME AXI-SYMMETRIC ISENTROPIC CENTREBODY INTAKES DESIGNED FOR MACH NUMBERS OF 2.48 AND 3.27	ARC R&M 3586 A CONVERGENT NOZZLE FOR THE STANDARDISATION OF THRUST-IG MEASUREMENTS	Next

Bound With Arc R&M-3580-3582,3584-3589.Lack No-3582

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