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MEASUREMENTS OF THE BOUNDARY LAYER AND WAKE OF TWO AEROFOIL SECTIONS AT HIGH REYNOLDS NUMBERS AND HIGH-SUBSONIC MACH NUMBERS.

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BookPublisher: Her Majesty'S Stationery Office, London 1973Description: 89.DDC classification: ARC | R&M 3722

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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 3722 (Browse shelf)	Not for loan		TR11166

Total holds: 0

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Previous	ARC R&M 3719 AN ITERATIVE METHOD FOR CALCULATION OF THE LOADING ON A THIN UNSWEPT WING.	ARC R&M 3720 AN EXPERIMENTAL INVESTIGATION OF THE SUBSONIC LONGITUDINAL CHARACTERISTICS OF FIVE SLENDER-WING MODELS WITH GOTHIC PLANFORMS.	ARC R&M 3721 THE LIFT AND STALLING CHARACTERISTICS OF A 35 DEG. SWEPT BACK WING DESIGNED TO HAVE IDENTICAL CHORDWISE PRESSURE DISTRIBUTIONS AT ALL SPANWISE STATIONS WHEN NEAR MAXIMUM LIFT.	ARC R&M 3722 MEASUREMENTS OF THE BOUNDARY LAYER AND WAKE OF TWO AEROFOIL SECTIONS AT HIGH REYNOLDS NUMBERS AND HIGH-SUBSONIC MACH NUMBERS.	ARC R&M 3723 OPTIMUM REINFORCEMENT AROUND A CIRCULAR HOLE IN A FLAT SHEET UNDER UNIAXIAL TENSION.	ARC R&M 492 National gas turbing establishment	ARC R&M 632 PRESSURE MEASUREMENTS ON A CONE-CYLINDER-FLARE CONFIGURATION AT SMALL INCIDENCES FOR M=6.8	Next

Bound With Arc R&M 3700-3721, 3723 Lack No. 3704,7-15.

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