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THE FLOW PRODUCED BY INTERACTION OF A TURBULENT BOUNDARY LAYER WITH A NORMAL SHOCK WAVE OF STRENGTH SUFFICIENT TO CAUSE SEPARATION

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BookPublisher: Her Majesty'S Stationery Office, London 1960Description: 21.DDC classification: ARC | R&M 3502

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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 3502 (Browse shelf)	Not for loan		TR16993

Total holds: 0

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Previous	ARC-R&M 3498 CALCULATION OF THE RESPONSE OF A FLEXIABLE AIRCRAFT TO HARMONIC AND DISCRETE GUSTS BY A TRANSFORM METHOD.	ARC-R&M 3499 LOW-SPEED MEASUREMENTS OF SKIN-FRICTION ON A SLENDER WING	ARC-R&M 3500 THE THEORY OF INTERFERENCE EFFECTS ON DYNAMIC MEASUREMENTS IN SLOTTED- WALL TUNNELS AT SUBSONIC SPEEDS AND COMARISONS WITH EXPERIMENT.	ARC R&M 3502 THE FLOW PRODUCED BY INTERACTION OF A TURBULENT BOUNDARY LAYER WITH A NORMAL SHOCK WAVE OF STRENGTH SUFFICIENT TO CAUSE SEPARATION	ARC R&M 3503 AERODYNAMIC LOADS ON EXTERNAL STORES	ARC R&M 3504 THE LINEARIZED FLOW OF A RELAXING GAS THROUGH A NON-UNIFORM CHANNEL AND IN A JET SUPERSONIC SPEEDS	ARC R&M 3505 EXPERIMENTS WITH CONES IN LOW-DENSITY FLOWS AT MACH NUMBERS NEAR 2	Next

Bound With Arc R&M-3501,3503-3510.

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