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MEASUREMENT OF THE YAWING MOMENT AND PRODUCT OF INTERTIA OF AN AIR CRAFT BY THE SINGLE POINT SUSPENSION METHOD

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BookSeries: Aeronautical Research Council Report And Memoranda 3607. Publisher: DDC classification: R&M-3607

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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-3607 (Browse shelf)	Not for loan		TR6130

Total holds: 0

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Previous	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	R&M3614 PILOTED SIMULATOR STUDY OF A STENDER-WING RESEARCH AIRCRAFT (HP-115)	R&M3620 MEASUREMENT OF THE MOMENTS AND PRODUCT OF INERTIA OF THE FAIREY DELTA 2 AIRCRAFT	R&M-3690 STUDY OF DYNAMIC AEROELASTIC EFFECTS ON THE STABILITY CONTROL AND GUST RESPONSE OF A SLENDER DELTA AIRCRAFT	Next

Bound With:Arc R&M 3602-3620

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