PKK Library Search for 'se,phr:"Aeronautical Research Council Current Papers"'

SOME RESULTS OF WIND-TUNNEL TESTS ON AN AEROFOIL SECTION (NPL 9510) COMBINING A'PEAKY' UPPER SURFACE-PRESSURE DISTRIBUTION WITH REAR LOADING

By Hall, D.J., Quincey, V.G.. , Bound With: Arccp-1291-1300

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INVESTIGATION IN TO THE DUTY CYCLE OF POWERED FLYING CONTRALS PARTS 1 AND 2

By Holoubeck, F.. , Bound With:Arc Cp No 1311-1320

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SLR TEMPERATURE MEASUREMENTS IN THE SUPERSONIC EXPANSION OF NITROGEN IN SHOCKTUNNEL

By Lewis, Michael J.. , Bound With: Arc Cp No.-1291-1300

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PREDICTION METHOS FOR PRESSURE DISTRIBUTIONS ON COMPRESSION SURFACES OF COMICAL BODIES AT SUPERSONIC SPEEDS

By Larpcombe,M.J.. , Bound With:Arc Cp No.1291-1300

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NON-LINEAR STABILITY THEORY OF THE FLAT PLATE BOUNDARY LAYER

By Corner, D., Barry, M.D.J.. , Bound With: Arc Cp No.1291-1300

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THRUST/ DRAG ANALYSIS FOR A FRONT FAN NACELLE HAVING TWO SEPARATE COAXIAL EXHAUST STREAMS

By Street, P. G.. , Bound With: Arc Cp No 1311-1320

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FINITE-DIFFERENCE SCHEME FOR COMPUTING SUPERCRITICAL FLOWS IN ARBITARY CO-ORDINATE SYSTEMS

By Albone, C. M.. , Bound With: Arc Cp No 1311-1320

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FATIGUE CRACK PROPAFATION IN THIN SHEETS OF L73 UNDER CONSTANT STRAIN AMPLLITUDE

By O' Neil, P. H.. , Bound With: Arc Cp No 1311-1320

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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

By Greenwood, G.H.. , Bound With: Arc Cp No 1311-1320

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OBSERVATION OF THE FLOW FORM A RECTANGULAR NOZZLE

By Kurn,A. G.. , Bound With: Arc Cp No.1311-1320

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

By Hutton, G. B., Drane, D.A.. , Bound With: Arc Cp No 1311-1320

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EFFECT OF LOAD DWELLS DURING FATIGUE CRACK PROPAGATION

By Kiddle, F.E. , Bound With: Arc Cp No 1311-1320

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INTERFERENCE PROBLEMS ON WING-FUSELAGE COMBINATIONS

By Weber, J.. , Bound With: Arc Cp-1331-1340

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INTERFERENCE PROBLEMS ON WING-FUSELAGE COMBINATIONS PART IV THE DESIGN PROBLEM FOR A LIFTING SWEPT WINNG ATTACHED TO A CYLINDRICAL FUSELAGE

By Weber, J.. , Bound With: Arc Cp-1331-1340

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MEASUREMENTS OF SECONDARY LOSS IN A MODEL TURBINE WITH VARIABLE INLET BOUNDARY LAYER

By Denton, J.D.. , Bound With:Arc Cp-1331-1340

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ASSESSMENT OF THE IMPORTANCE OF THE RESIDUAL FLEXIBILITY OF NEGLECTED MODES IN THE DYNAMICAL ANALYSIS OF DEFORMABLE AIRCRAFT

By Taylor, A. S.. , Bound With: Arc Cp 1331-1340

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DESIGN AND THEORETICAL ASSESSMENT OF EXPERIMENT GLIDE PATH AND FLARE SYSTEMS FOR A BAC 1-11 AIRCRAFT (INCLUDING DIRECT LIFT CONTROL

By Gill, F.R.. , Bound With: Arc Cp-1331-1337

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INFLUENCE OF FIBRE WAVINESS ON THE MODULI OF UNIDIRECTIONAL FIBRE REINFORCED COMPOSITES

By Mansfield, E.H.. , Bound With: Arc Cp 1331-1340

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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 ...

By Wigley,T.G.. , Bound With:Arc Cp-No.1340

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GUST LOADS ON 707 AND VC 10 AIRCRAFT

By Keynes,I. W.. Her Majestys Stationery Office, London 1974 . 16 , Bound With: Arc Cp No.1281-1290

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APPLICATION OF A VARIATIONAL METHOD IN PLANE COMPRESSIBLE FLOW CALCULATION

By Rasmussen,H.. Her Majestys Stationery Office, London 1974 . 24 , Bound With: Arc Cp No.1281-1290

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SOME PREDICTIONS OF CRACK PROPAGATION UNDER COMBINED CABIN PRESSURISATION AND ACOUSTIC LOADINGS

By Kirkby,W. T.. Her Majestys Stationery Office, London 1974 . 22 , Bound With: Arc Cp No.1281-1290

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CIVIL AIRCRAFT AIRWORTHINESS DATA RECORDING PROGRAMME UNEVEN RUNWAYS ENCOUNTERED BY SUBSONIC JET TRANSPORT AIRCRAFT DURING SCHEDULED AIRLINE OPERATIONS

By Hutton,G. B.. Her Majestys Stationery Office, London 1974 . 16 , Bound With: Arc Cp No.1281-1290

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AEROELASTIC MODEL HELICOPTER ROTOR

By Cansdale,R.. Her Majestys Stationery Office, London 1974 . 14 , Bound With: Arc Cp No.1281-1290

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STUDY OF SOLID STATE REMOTE CONTROL TECHNIQUES AS APPLIED TO THE REDESIGN OF THE ELECTRICAL SYSTEM IN A LARGE CIVIL AIRCRAFT

By Jones,L.V.C.. Her Majestys Stationery Office, London 1974 . 54 , Bound With: Arc Cp No.1281-1290

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SHOCK CAPTURING METHOD FOR CALCULATING SUPERSONIC FLOW FIELDS

By Walken,F.. Her Majestys Stationery Office, London 1974 . 29 , Bound With: Arc Cp No. 1281-1290

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MEASUREMENT OF THE ITERNAL PERFORMANCE OF A RECTANGULAR AIR INTAKE MOUNTED ON A FUSELAGE AT MACH NUMBERS FROM 1.6 TO 2

By Brown,C. S.. Her Majestys Stationery Office, London 1974 . 18,IV , Bound With: Arc Cp 1291-1300

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LOW-SPEED WIND-TUNNEL TESTS ON THE LIFT-DEPENDENT DRAG OF DELTA WINGS WITH CONICAL CAMBER

By Kirkpatrick,D.L.T.. Her Majestys Stationery Office, London 1974 . 26 , Bound With: Arc Cp No.1291-1300

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VARIABILITY OF FATIGUE DAMAGE FROM FLIGHT TO FLIGHT

By Bullen,N. I.. Her Majestys Stationery Office, London 1974 . 23 , Bound With: Arc Cp No.1291-1300

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FLIGHT DETERMINATION OF THE RUDDER POWER AND DIRECTIONAL STABILITY OF THE FAIREY DELTA 2 AIRCRAFT USING A WINGTIP PARACHUTE

By Ingle,G.. Her Majestys Stationery Office, London 1974 . 21 , Bound With: Arc Cp No.1291-1300

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FLIGHT SIMULATION OF A WESSEX HELICOPTER A VALIDATION EXERCISE

By Wilcock,T.. Her Majestys Stationery Office, London 1974 . 41 , Bound With: Arc Cp No.1291-1300

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LIST OF CURRENT PAPERS

Her Majestys Stationery Office, London 1974 . 5 , Bound With: Arc Cp No.1291-1300

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PEREDICTION OF HELICOPTER ROTOR HOVER PERFORMANCE USING A PRESCRIBED WAKE ANALYSIS

By Young,C.. Her Majestys Stationery Office, London 1976 . 30 , Bound With: Arc Cp No.1341-1350

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PILOTED FLILGHT SIMULATION OF THE WEST AND LYNX

By Wilcock,T.. Her Majestys Stationery Office, London 1976 . 55 , Bound With: Arc Cp No.1341-1350

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THEORETICAL INVESTIGATION OF HIGH SPEED AXISYMMETRIC TURBULENT MIXING LAYERS WITH LARGE TEMPERATURE DIFFERENCES

By Carpenter,P. W.. Her Majestys Stationery Office, London 1976 . 26 , Bound With: Arc Cp No. 1341-1350

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MEASUERMENT OF THE INTERNAL PERFORMANCE OF A RECTANGULAR AIR-INTAKE AT A MACH NUMBER OF 0.9

By Brown,C. S.. Her Majestys Stationery Office, London 1976 . 12 , Bound With: Arc Cp No.1341-1350

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NUMERICAL METHODS FOR CALCULATING UNSTEADY FLOWS IN SUBSONIC AND SUPERSONIC TURBOMACHINERY CASCADES

By Hobson,D. E.. Her Majestys Stationery Office, London 1976 . 13 , Bound With: Arc Cp-1341-1350

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EFECT OF GEOMETRY ON THE FATIGUE STRENGTH OF ALUMINIUM ALLOY LUNGS

By Kiddle,F. E.. Her Majestys Stationery Office, London 1976 . 7 , Bound With: Arc Cp No.1341-1350

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NUMBERS 1301-1350

Her Majestys Stationery Office, London 1977 . 6 , Bound With: Arc Cp 1342-1350

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TWO-DIMENSIONAL AEROFOIL OSCILLATING AT LOW FREQUENCIES IN HIGH SUBSONIC FLOW

By Nixon,D.. Her Majestys Stationery Office, London 1974 . 49 , Bound With: Arc Cp No.1281-1290

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STUDY OF THERMAL FATIGUE ACCLERATION IN BOX BEAMS UNDER MECHANICAL AND THERMAL STRESS

By Kiddle,F. E., Kite,R. J.. Her Majestys Stationery Office, London 1976 . 31 , Bound With: Arc Cp No.1341-1350

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LIST OF CURRENT PAPERS NUMBERS 601-650

Her Majestys Stationery Office, London 1964 . 5 , Bound With: Arc-Cp No. 650-1223

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FORTRAN SUBROUTINES FOR FINITE ELEMENT ANALYSIS

By Merrifield,B. C.. Her Majestys Stationery Office, London 1972 . 28 , Bound With: Arc-Cp No.650-1223

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CHARACTERISTICS OF A FAMILY OF ROOFLAP AEROFOILS DESIGNED AT THEIR DRAG-RISE CONDITION IN VISCOUS, COMPRESSIBLE FLOW

By Thompson,B.G.T., Cosby,S. W.. Her Majestys Stationery Office,London 1975 . 15,II , Bound With: Arc Cp 1321-1330

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NON-AXISYMMETRIC END-WALL BOUNDARY LAYER THEORY FOR AXIAL COMPRESSOR ROWA

By Railly,J. W.. Her Majestys Stationery Office, London 1975 . 20 , Bound With: Arc Cp 1321-1330

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DEVELOPMENTS IN THE LIFTING SURFACE THEORY TREATMENT OF SYMMETRIC PLANFORMS WITH A LEADING EDGE CRANK IN SUBSONIC FLOW

By Hewitt,B. L.. Her Majestys Stationery Office, London 1975 . 31 , Bound With: Arc Cp 1321-1330

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ASSESSMENT OF THE ACCURACY OF SUBSONIC LINEARIZED THEORY FOR THE DESIGN OF WARPED SLENDER WINGS

By Davies,Patricia J.. Her Majestys Stationery Office, London 1975 . 26 , Bound With: Arc Cp 1321-1330

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SYSTEMS OF COORDINATES SUITABLE FOR THE NUMERICAL CALCULATION OF THREE-DIMENTIONAL FLOW FIELDS

By Mangler,K. W.. Her Majestys Stationery Office, London 1975 . 68 , Bound With: Arc Cp 1321-1330

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LOW-SPEED WIND TUNNEL TESTS OF A TWO DIMENSIONAL WING FITTED WITH TWO PLAIN DIFFERENTIALLY-DEFLECTED TRAILING-EDGE FLAPS

By Mckie,John. Her Majestys Stationery Office, London 1975 . 19 , Bound With: Arc Cp 1321-1330

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THEORY OF PRACTICAL RETRACTION OF IMPERFECTLY ELASTIC ROPES

By Stevens,G. W.H.. Her Majestys Stationery Office, London 1975 . 12 , Bound With: Arc Cp 1321-1330

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UREA FORMALDEHYDE FOAMED PLASTIC EMERGENCY ARRESTERS FOR CIVIL AIRCRAFT

By Gwynne,G. M.. Her Majestys Stationery Office, London 1975 . 42 , Bound With: Arc Cp 1321-1330

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