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DESIGN AND OPERATION OF THE X-15 HYPERSONIC RESEARCH AIRPLANE.

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BookPublisher: North Atlantic Treaty Organization, Paris 1960Description: 31.DDC classification: NATO | AGARD-288

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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-288 (Browse shelf)	Not for loan Untraceable		TR12220

Total holds: 0

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Previous	NATO AGARD-279 EFFECTS OF HEAT TRANSFER ON LAMINAR BOUNDARY LAYER DEVELOPMENT UNDER PRESSURE GRADIENTS IN COMPRESSIBLE FLOW.	NATO AGARD-281 TURBULENT BOUNDARY LAYERS WITH HEAT TRANSFER IN COMPRESSIBLE FLOW.	NATO AGARD-282 REAL-GAS LAMINAR BOUNDARY LAYER SKIN FRICTION AND HEAT TRANSFER.	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.	Next

Bound With Nato Agard-200-287,289-297.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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