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List of Current Papers Numbers 651-700

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List of Current Papers Numbers 651-700 C.P. No. 700 LJ!GFdARY @QX4L AIRCRAFT ESTABLISHMENT 6EQFORR MINISTRY OF AVIATION AERONAUTICAL RESEARCH COUNCll CURRENT PAPERS List of Current Papers Numbers 651-700 LONDON: HER MAJESTY’S STATIONERY OFFICE 1965 Price 1s. 6d. net List of Current Papers Published for THE AERONAUTICAL RESEAPCH COUNCIL (Numbers 651-700) and placed on sale by H.M. Stationery Office C.P. No. Council No. Title Author(s) 651 24 189 Unsteady lift slope values obtained Ridland, D. M. from flight measurements in gusts. (June, 1962). 652 24 245 The static and dynamic response Pinsker, W.J.G. properties of incidence vanes with aerodynamic and internal viscous damping. (August, 1962). 653 23 046 Flight measurements of the Dutch Rose R. roll chsracterlstics of a 60 degree delta wing aircraft (Fairey Delta 2) at Mach numbers from O-4 to 1.5 with stability derivatives extracted by vector analysis. (March, 1961). 654. 23 976 The calwlation of the velocity HaLnes, A. B., dztnbution due to thickness Rollins, K. and for swept wings with subsonic Osborn, J. edges at supersonic speeds. (June, I 962) 655 23 573 Propagation of fatigue cracks in Raithby, K. D. wide unstiffened aluminium alloy and sheets. Bebb, Marie E. (September, 1961). 66 UC 740 8 ft x 6 ft transonic wind tunnel Kettle, D. J. tests on a l/24 scale model of the Faxey Delta 2 (ER.103). (May, 1962). 657 23 691 Pressure measurements on a cone- Peckham, D. H. cylinder-flare configuration at M = 6'85 and incidences up to 30°. (January, 1962). -2- C.P. No. Council No. Title Author(s) 658 u, 280 Proving tests of a wingtip Dee, F. W. parachute installation on a Venom aircraft, with some measurements of directional stability and ruaaer power. (JUIX, 1962). 659 23 791 Slender not-so-thin ting theory. Cooke, J. C. (Jmwy, 1962). 660 u, 346 Room temperature instability and Waldren, N. E. fraction in rotating discs and and correlation with bi-axial tensile b-a, D. E. test data. (January, I 963). 661 7% 587 The influence of a wide hub on the Walclren, N. E. room temperature burst strength and of model steam turbine rotors. Ward, D. E. (March, 1963). 662 23 777 An empirical prediction method for Collxxgbourne, J.R. non-linear normal force on thin wings at supersonic speeds. (January, 1962). 663 24 647 The 7 in. x 7 m. hypersonio wind Crane, J. F. W. tunnel at R.A.E. Farnborough ana Pert IV - Measurements of diffuser Woodley, J. C. performance, blockage, starting loads and humidity. (December, 1962). 664 23 160 Estxnation of stability derivatives Thomas, H.H.B.M. State of the art). t August, 1961). 665 24 396 A note on the generalisation of Lester, W. G. S. elastic curves representing parachute shapes. (July, 1962). 666 23 963 Fatigue behaviour under service and Wlnkworth, W. J. ground test conditions (A oomparlson based on the Dakota Wing). (November, 1961). 667 u, 847 Annual varlatlon of flight loads Taylor, R. Hain recorded on Viscount aircraft by means of the fatigue lod meter. (December, 1962). 668/ -3- C.P. No. Council No. Title Author(s) 668 19 665 Aeroalastic problems of high speed Moxor., D. acLrcraft. (May, 1957). 24 221 Side force on a wug body combination Barnes, J. R. due to trailing vortices. (July, 1962). 670 24 446 Free-flight measurements of the Edwards, J.B.W. zero-ldt drag of a slender ogee wmg at transonic and supersonic speeds. (October, I 962). 671 24 445 Inflatable servo actuators. Mettam, A. R. (October, I 962). 672 24 606 Wind tunnel tests at supersonic Dobson, M. D. speeds on a model of the Fairey Delta 2. (October, I 962). 673 24 570 Measurement of lift and pltching Squire, L. C. moment on four ogee wings at supersonic speeds. (October, 1962). 674 22 515 Forces on tethered ballistic Moxon, D. mxssdes due to motor cut-off - A theoretlcal treatment. (August, 1960). 675 24 437 Calculated lift cllstrlbutlons in Bagley, J. A. lncoppresslble flow on some and sweptback wings. Joyce, G. M. (Au@st, I 962). 676 24 504 Low altitude gust measurements Wells, E. W. over three routes in the U.K. (October, 1962), 677 23 a03 The evaluation of some commercial Stevens, D. R. and development pressure gauges in a laboratory type shock tube with a vxew to thev suItabIlity for use in shock tunnels. (Much, 1962). 678 20 997 Free-flqht model drag measurements Greenwood, G. H. on a transonw fighter (Gloster Javelin). (November, 1958). , 679/ -4- C.P. No. Council No. I Title I Author(s) 679 20 388 A roll-balance free-flight test Turner, K. J. vehicle for the measurement of aderon rolling power and roll damping at M = 0.8 to 2.5. / (March, 1958). 680 23 518 On the extrapolation and scatter Walles, K. F. A. I of creep data. ~ s.w.3 (October, 1961). Graham, A. 681 23 640 The comparison of theory and Acum,W.E.A. experiment for oscillating Tt%, 1962). 682 23 847 !Che effect of an initialboundsry Nash, J. F. layer on the development of a turbulent free shear layer. (June, 1962). 683 23 907 A note on the use of end plates Condrey, C. F. to prevent three-dimensional flow at the ends of bluff cylinders. (June, 1962). 23 945 Preliminary measurements in .a Pennelegion, L. shook tunnel of shook angle and and undersurface pressure Cash, R. F. related to a FFonweiler wing. (July, 1962). 685 23 977 A time-divulon analogue Johnson, R. F. multiplier for correlation measurements and mixing at frequencies up to 100 kilocycles per second. (August, 1962). 686 23 899 A simplified treatment of Stratford, B. S. losses for one-dimensional and axing between hot and cold Williams, J. G. gas streams at constant pressure and low velocity. (June, 1962). 687/ -5- C.P. No. Counc~.l No. Title Author(s) 687 23 947 The mixing with ambient air of a Stratford, B. S., cold airstream in a centrifugal Jawor, Z. M. field. and (June, 1962). Golesworthy, G. T. 688 24 384 On theoretical plasticity and Mansfield, E. H. crack propagation. (August, 1962). 689 24 742 Power spectra of the vertical Burns, A. component of atmospheric turbulence obtained from concurrent measurements on an aircraft and at fixed points. (January, 1963). 23 712 On the effect of fan and Gregory, N. thrust engine loading on the transition peer requirements of a fan wing. (April, 1962). 691 24 367 On the numerical calculation Thwaites, B. of Theodorsen's transformation. (January, 1963). 692 23 974 Tensile instability of hollow Mellor, P. B. rotating discs of uniform and thickness. Percy, M. J. (July, I 962) (Mod. Jan. ‘63). 693 24 027 Tunnel tests on a double cascade Stratford, B. S. to deterrmne the interaction end between the rotor and the Sansome, G. E. nozzles of a supersonic turbine. (August, 1962). 694 24 222 Boundary lsyer characteristics ~ Catherall, D. of caret wings. (day, 1963). 695 24 537 Pltohing derivatives for & Garner, H. C. gothic wing oscillating about and a mean xd.dence. Doris E. Lehrian. (February, 1963). 6% 24 884 Turbulent boundary layers on Cooke, J. C. delta wings at zero lift. @arch, 1963). 697/ -6- C.P. No. Council No. Title I Author(s) I 697 24 247 Two-dimensiocal separated or Gada, G. E. cavitating flow past a flat plate normalto the stream. (November, 1962). 698 24 722 The pressure oalibration of the Cm, S. G., R.A.E. 6 in. diameter shock Pallant, R. J. tube with .a view to its use as and the driver of a cold Shaw, J. M. high-density hypersonic tunnel. (April, 1963). 699 24 739 The boundary layer drag of Cooke, J. C. bodies with swept trailing edges in supersonic flow. (February, 1963). 700 List of Current Papers published for the Aeronautical Research Council. (Nos. 651-700). DS. C.P. No. 700 0 Crown copyrrght 1965 Prmted and pubhshed by HER MAJESTY’S STATIONERY OFFICE To be purchased from York House, Kmgsway, London w c 2 423 Oxford Street, London w 1 13~ Castle Street, Edmburgh 2 109 St Mary Street, Cardlff 39 Kmg Street, Manchester 2 50 Farfax Street, Bristol 1 35 Smallbrook, Rmgway, Blrmmgham 5 80 ChIchester Street, Belfast 1 or through any bookseller Printed m England I C.P. No. 700 SO Code No. 23.9015 .
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