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SOME EFFECTS OF WIND TUNNEL INTERFERENCE OBSERVED IN TESTS ON TWO-DIMENSIONAL AERFOLIS AT HIGH SUBSONIC AND TRANSONIC SPEEDS.

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BookPublisher: North Atlantic Treaty Organization, Paris 1959Description: 61.DDC classification: NATO | AGARD-296

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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	NATO AGARD-296 (Browse shelf)	Not for loan Untraceable		TR12223

Total holds: 0

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Previous	NATO AGARD-288 DESIGN AND OPERATION OF THE X-15 HYPERSONIC RESEARCH AIRPLANE.	NATO AGARD-293 SOME APPLICATIONS OF TRANSONIC-FLOW THEORY TO PROBLEMS OF WIND-TUNNEL INTERFERENCE.	NATO AGARD-294 THE EFFECTIVENESS OF THE TRANSONIC WIND-TUNNEL AS A DEVICE FOR MINIMIZING TUNNEL-BOUNDARY INTERFERENCE FOR MODEL TESTS AT TRANSONIC SPEEDS.	NATO AGARD-296 SOME EFFECTS OF WIND TUNNEL INTERFERENCE OBSERVED IN TESTS ON TWO-DIMENSIONAL AERFOLIS AT HIGH SUBSONIC AND TRANSONIC SPEEDS.	NATO AGARD-297 AN INVESTIGATION OF INTERFERENCE EFFECTS ON SIMILAR MODELS OF DIFFERENT SIZE IN VARIOUS TRANSONIC TUNNELS IN THE UK.	NATO AGARD-3 AIRCRAFT STRUCTURES RESEARCH AT ELEVATED TEMERATURES	NATO AGARD-301 LARGE ANGLE OF ATTACK MODEL-STING INTEFERENCE EFFECTS AT TRANSONIC SPEEDS.	Next

Bound With Nato Agard-200-295,296-297.Lack No-201-2,4,24,226-60,62,64-66,68-69,72-74,76,80,83-87,89-92,95.

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