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AN EXPERIMENTAL INVESTIGATION OF THE EFFECT OF PLANFORM SHAPE ON THE SUBSONIC LONGITUDINAL STABILITY CHARACTERISTICS OF SLENDER WINGS

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BookPublisher: Her Majesty'S Stationery Office, London 1969Description: 85.DDC classification: ARC | R&M 3568

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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 3568 (Browse shelf)	Not for loan		TR17051

Total holds: 0

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Previous	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	ARC R&M 3569 STATIC INSTABILITY OF RECTANGULAR ORTHOTROPIC PANELS SUBJECTED TO UNIFORM IN-PLANE LOADS AND DEFLECTION-DEPENDENT LATERAL LOADS	ARC R&M 3571 LOW-SPEED WIND-TUNNEL TESTS ON THE EFFECTS OF TAIPLANE AND NACELLE POSITION ON THE SUPERSTALL CHARACTERISTICS OF TRANSPORT AIRCRAFT	ARC R&M 3572 THE SUBERITICAL RESPONSE AND FLUTTER OF A SLENDER WING MODEL AIRCRAFT	Next

Bound With Arc R&M 3561-3567, 3569, Lack No.3564

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