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MEASUREMENTS OF OSCILLATORY AERODYNAMIC HINGE MOMENTS FROM THE RESPONSE OF A WIND TUNNEL MODEL TO TURBULENT FLOW

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Material type: Text

TextSeries: Aeronautical Research Council Current Papers ; Cp No.1317Publication 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-1317 (Browse shelf(Opens below))	Not for loan		TR3334

Total holds: 0

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Previous	CP1314 FATIGUE CRACK PROPAFATION IN THIN SHEETS OF L73 UNDER CONSTANT STRAIN AMPLLITUDE	CP-1315 FREE-FLIGHT MODEL DYNAMIC STABILITY MEASUREMENTS ON A `NOT SO SLENDER' WING/FIN COMBINATION AT ZERO AND SMALL LIFT, M=0.8 TO 2.0	CP-1316 OBSERVATION OF THE FLOW FORM A RECTANGULAR NOZZLE	CP-1317 MEASUREMENTS OF OSCILLATORY AERODYNAMIC HINGE MOMENTS FROM THE RESPONSE OF A WIND TUNNEL MODEL TO TURBULENT FLOW	CP1318 EFFECT OF LOAD DWELLS DURING FATIGUE CRACK PROPAGATION	CP-1319 THEORETICAL AND EXTERNAL-FLOW, JETAUGMENTED FLAP	CP-1320 THE CHARACTERISTICS OF A FAMILY OF ROOFTOP AEROFOLSDESIGNED AT THEIR DRAG RISE CINDITION IN VISCOUS, CIMPRESSIBLE FLOW PART1	Next

Bound With: Arc Cp No 1311-1320

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