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ON THREE- DIMENSIONAL BODIES OF DELTA PLANFORM WHICH CAN SUPPORT PLANE ATTACHED SHOCK WAVES

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BookPublisher: Her Majesty'S Stationery Office, London 1963Description: 12.DDC classification: ARC | CP 640

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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 CP 640 (Browse shelf)	Not for loan Untraceable		TR17118

Total holds: 0

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Previous	ARC CP 637 THEORETICAL COMPARISON OF THE FLOW OVER A FLAT DELTA WING AND A RECTANGULAR PYRAMID	ARC CP 638 SURFACE PRESSURES AND STRUCTURAL STRAINS RESULTING FROM FLUCTUATIONS IN THE TURBULENT BOUNDARY LAYER OF A FAIREY DELTA 2 AIRCRAFT.	ARC CP 639 MEASUREMENTS IN FLIGHT OF THE LONGITUINAL STABILITY DERIVATIVES OF A 60 DEGREE DELTA WING AIRCRAFT(FAIREY DELTA 2)	ARC CP 640 ON THREE- DIMENSIONAL BODIES OF DELTA PLANFORM WHICH CAN SUPPORT PLANE ATTACHED SHOCK WAVES	ARC CP 641 PRESSURE MEASURENETS AT SUPERSONIC SPEEDS ON THREE UNCAMBERED CONICAL WINGS OF UNIT SAPECT RATIO	ARC CP 642 THE EFFECT OF SKIN TAPER ON THE AEROELASTIC PROPERTIES OF WINGS	ARC CP 643 LOW SPEED WIND TUNNEL TESTS ON A KITE BALLOON MODEL	Next

Bound With Arc Cp- 631-639,641-649.

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