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THE SUBERITICAL RESPONSE AND FLUTTER OF A SLENDER WING MODEL AIRCRAFT

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BookPublisher: Her Majesty'S Stationery Office, London 1969Description: 34.DDC classification: ARC | R&M 3572

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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 3572 (Browse shelf)	Not for loan		TR17011

Total holds: 0

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Previous	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	ARC R&M 3574 HEAT TRANSFER AND TRANSITION MEASUREMENTS AT M=8.5 ON A DELTA MODEL AND A FLAT PLATE AT INCIDENCE	ARC R&M 3575 THE RESPONSE OF A CONSTANT-PRESSURE TURBULENT BOUNDARY LAYER TO THE SUDDEN APPLICATION OF AN ADVERSE PRESSURE GRADIENT	ARC R&M 3576 A MOMENTUM ANALYSIS OF LIFTING SURFACES IN INVISCID SUPERSONIC FLOW	Next

Bound With Arc R&M 3570-3571, 3574-3579, Lack No. 3573

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