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ON THE FLOW IN A REFLECTED-SHOCK TUNNEL

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BookPublisher: Her Majesty'S Stationery Office, London 1962Description: 34.DDC classification: ARC | R&M 3265

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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 3265 (Browse shelf)	Not for loan Untraceable		TR17105

Total holds: 0

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Previous	ARC-R&M 3260 A PROPOSED APPARATUS FOR MEASURING OSCILLATORY AERODYNAMICS DERIVATIVES.	ARC R&M 3263 MEASUREMENTS OF LIFT AND GROUND INTERFERENCE ON A LIFTING-FAN WING AT ZERO FORWARD SPEED	ARC R&M 3264 WIND TUNNEL TESTS AND THEORETICAL INVESTIGATIONS ON THE EFFECT OF A LOCALISED MASS ON THE FLUTTER OF A DELTA WING WITH FIXED ROOT	ARC R&M 3265 ON THE FLOW IN A REFLECTED-SHOCK TUNNEL	ARC R&M 3266 STRESSE PRODUCED IN AN INFINITE ELASTIC PLATE BY THE APPLICATION OF LOADS TRAVELLING WITH UNIFORM VELOCITY ALONG THE BOUNDING SURFACES	ARC R&M 3267 THE EFFECT OF TEMPERATURE VARIATIONS IN THE PLANE AND THROUGH THE THICKNESS OF A CIRCULAR LENTICULAR PLATE	ARC R&M 3268 EFFECTS OF WING STIFFNESS AND INERTIA CHANGES ON THE MODES AND FREQUENCIES OF A MODEL DELTA AIRCRAFT	Next

Bound With Arc R&M3262-64,3266-70 Lack No.3269

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