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PRE-FLIGHT SIMULATION OF THE B.A.C. 221 SLENDER WING RESEARCH AIRCRAFT

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BookSeries: Aeronautical Research Council Report And Memoranda 3582. Publisher: DDC classification: R&M-3582

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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	R&M-3582 (Browse shelf)	Not for loan		TR6127

Total holds: 0

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Previous	R&M3099 THERMODYNAMIC DATA FOR THE CALCULATION OF GAS TURBINE PERFORMANCE	R&M3562 SCHEME OF NOTATION AND NOMENCLATURE FOR AIRCRAFT DYNAMICS AND ASSOCIATED AERODYNAMICS	R&M3573 FORMULATION OF ON INFLUENCE- COEFFICIENT METHOD FOR DETERMMINING STATIC AEROELASTIC EFFECTS,AND --- APPLICATION TO A SLENDES AIRCROFT IN SYMMETRIC FLI	R&M-3582 PRE-FLIGHT SIMULATION OF THE B.A.C. 221 SLENDER WING RESEARCH AIRCRAFT	R&M-3602 LANDING FLARE OF LARGE TRANSPORT AIRCRAFT	R&M-3606 REVIEW OF RECENT RESEARCH ON HANDLING QUALITIES AND ITS APPLICATION TO THE HANDLING PROBLEMS OF LARGE AIRCRAFT	R&M-3607 MEASUREMENT OF THE YAWING MOMENT AND PRODUCT OF INTERTIA OF AN AIR CRAFT BY THE SINGLE POINT SUSPENSION METHOD	Next

Bound With:Arc R&M 3573-3582

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