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BOUNDARY-LAYER INTERACTION EFFECTS IN INTAKES WITH PARTICULAR REFERENCE TO THOSE DESIGNED FOR DUAL SUBSONIC AND SUPERSONIC PERFORMANCE

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BookPublisher: Her Majesty'S Stationery Office, London 1970Description: 22.DDC classification: ARC | R&M 3565

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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 3565 (Browse shelf)	Not for loan		TR17048

Total holds: 0

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Previous	ARC R&M 3559 COMPARATIVE THEORETICAL CALCULATIONS OF FORCES ON OSCILLATING WINGS THROUGH THE TRANSONIC SPEED RANGE	ARC R&M 3562 A SCHEME OF NOTATION AND NOMENCLATURE FOR AIRCRAFT DYNAMICS AND ASSOCIATED AERODYNAMICS	ARC R&M 3563 THE SPEED RESPONSE OF AN AIRCRAFT CONSTRAINED TO FLYALONGA STRAIGHT PATH IN THE PRESENCE OF TURBULENCE AT LOW ALTITUDE	ARC R&M 3565 BOUNDARY-LAYER INTERACTION EFFECTS IN INTAKES WITH PARTICULAR REFERENCE TO THOSE DESIGNED FOR DUAL SUBSONIC AND SUPERSONIC PERFORMANCE	ARC R&M 3566 A FLIGHT SIMULATOR FOR RESEARCH INTO AIRCRAFT HANDLING CHARACTERISTICS	ARC R&M 3567 A GENERAL METHOD OF STUDYING STEADY LIFT INTERFERENCE IN SLOTTED AND PERFORATED TUNNELS	ARC R&M 3568 AN EXPERIMENTAL INVESTIGATION OF THE EFFECT OF PLANFORM SHAPE ON THE SUBSONIC LONGITUDINAL STABILITY CHARACTERISTICS OF SLENDER WINGS	Next

Bound With Arc R&M 3561-3563, 3566-3569, Lack No.3564

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