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EVALUATION OF A LIADING FORM FOR THE CALCULATION OF LINEARISED THEORY PRESSURE DISTRIBUTIONS ON WINGS WITH COUNTROL SURFACES HAVING SWEPT HINGE ...

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Material type: Text

TextSeries: Aeronautical Research Council Current Papers ; Cp No.1340Publication details: DDC classification:

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Holdings
Item type	Current library	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	CP-1340 (Browse shelf(Opens below))	Not for loan		TR3356

Total holds: 0

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Previous	CP-1320 THE CHARACTERISTICS OF A FAMILY OF ROOFTOP AEROFOLSDESIGNED AT THEIR DRAG RISE CINDITION IN VISCOUS, CIMPRESSIBLE FLOW PART1	CP1336 ASSESSMENT OF THE IMPORTANCE OF THE RESIDUAL FLEXIBILITY OF NEGLECTED MODES IN THE DYNAMICAL ANALYSIS OF DEFORMABLE AIRCRAFT	CP-1339 INFLUENCE OF FIBRE WAVINESS ON THE MODULI OF UNIDIRECTIONAL FIBRE REINFORCED COMPOSITES	CP-1340 EVALUATION OF A LIADING FORM FOR THE CALCULATION OF LINEARISED THEORY PRESSURE DISTRIBUTIONS ON WINGS WITH COUNTROL SURFACES HAVING SWEPT HINGE ...	CP1381 SHEAR PROPERTIES OF UNIDIRECTIONAL CARBON FIBRE REINFORCED PLASTICS AND THEIR EXPERIMENTAL DETERMINATION	CP-1393 THE CALCULATION,BY A FINITE DIFFERENCE METHOD,OF SUBCRITICAL FLOW WITHOUT CIRCULATION PAST A SWEPT ELLIPTIC CYLINDER BETWEEN WALLS	CR-2535 Computer analysis of multicircuit shells of revolution by the field method	Next

Bound With:Arc Cp-No.1340

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