Reports recommended by Council for publication which have not been included in Annual Technical Reports: Effect of Condensation of Atmospheric Water Vapour on Total Head and Other Measurement in NPL High Speed Tunnels, H.H.PEARCEY; Interpretation of Readings of Pitot and Static Tubes in High speed Tunnel in Which Condensation of Moisture Is Taking Place, C.N.H.LOCK. (R and M 2249); Integrating Comb Method as Applied to Profile Drag Results in Compressed Air Tunnel, D.H.WILLIAMS (R and M 2318); Two-Dimensional Supersonic Tunnel Interference, W.F.HILTON (R and M 2332); Structural and Aerodynamic Effects of Wing Thickness and Fuselage Size Variation, A. G.PUGSLEY, W. TYE, H.J.ALLWRIGHT (R and M 2377); Effect of Compressibility on Static Heads, C.N.H.LOCK, A.E.KNOWLER, H.H. PEARCE Y (R and M 2386); Installation of Engine Nacelle on Wing, R.SMELT, A. G.SMITH, F.SMITH, B.DAVISON (R and M 2406); Solution of Laminar Boundary layer Equation for Retarded Flow, D.R.HARTREE (R and M 2426); Profile drag Measurements at Compressibility Speeds on Aerofoils With and Without Spanwise Wires or Grooves, H.H.PEARCEY: Reynolds and Mach Number Effects on Pressure Distribution on Tail of EC 1250, J.A.BEAVAN (R and M 2252); Aerofoil Designed to Give Laminar Flow over Whole Surface with Boundary layer Suction, E.J.RICHARDS, C.H.BUR GE (R and M 2263); Experiments on NACA 23021 Aerofoil with 15% Handley Page Slotted Flap in Compressed Air Tunnel, D.H.WILLIAMS, A. F.BROWN (R and M 2305); Effect of Compressibility on Profile Drag of Aerofoils at Subsonic Mach Numbers in Absence of Shock Waves, A.D.YOU NG, N.E.WINTERBOTTOM (R and M 2400); Response of Aeroplane to Application of Elevators, L.W.BRYANT, R.W.G.GANDY (R and M 2275); Experiments on 20% Control with Tab, fitted to NACA 0015 Aerofoil -- Effect of Its Section on Hinge Moment and Lift, A.S.BATSO N, J.S.WARSAP, T.W.BROWN (R and M 2314); Low speed Model Tests on Effect of Nose and Gap Details on Elevator Characteristics, J.E.ADAMS ON, E.G.BARNES (R and M 2326); Flight Tests to Investigate Lightness of Unbalanced Elevator on Lockheed 12A, M.B.MORGAN, D.E.MORRIS (R and M 2372); Handling Tests on Curtiss H-75, and Comparative Aileron Tests on Curtiss H-75, Spitfire and Gloster F.5/34, M.B.MORGAN, D.E.M ORRIS, F.J.BIGG (R and M 2379); "Scissors Type" of Dynamic Balance for Control Surfaces, R.A.FRAZER (R and M 2369); Collected Researches on Stability of Kites and Towed Gliders, L.W.BRYANT, W.S.B ROWN, N.E.SWEETING (R and M 2303); Design of Parachutes for Large Bombs, W.D.BROWN, K.HARRISON (R and M 2324); Side and Floor Aperture Jumping, G.W.CARLING (R and M 2395); Dog Fight, S.B.GATES (R and M 2381); Relation Between Turning and Straight Performance, S.B.GATES (R and M 2382); Model Tests of "Return-flow" Cooling Scheme, Having Wing Leading Edge Entry and Nose-Slot Exit, R.SMELT, F.SMITH (R and M 2403); Lateral Response Theory, K.MITCHELL; Appendices by E.M.FRAYN (R and M 2297); Longitudinal Stability of Twin engined Monoplane with Airscrews Running, L.W. BRYANT, G.A.McMIL LAN (R and M 2310); Messerschmitt Me. 109 Handling and Manoeuvrability Tests, M.B.MORGAN, D.E. MORRIS (R and M 2361); Research Handling Tests on Blenheim L6595, M.B.MORGAN (R and M 2348); Turning Performance of Spitfire as Affected by Altitude and Flaps, M.B.MORGAN, D.E.MORRIS (R and M 2349). (£ 6.6s)


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    Title :

    Technical report of Aeronautical Research Council. Special volume 1


    Additional title:

    Technical Report of Aeronautical Research Council



    Publication date :

    1956


    Size :

    684 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




    Technical report of Aeronautical Research Council

    Engineering Index Backfile | 1955


    Technical report / Aeronautical Research Committee

    Großbritannien, Aeronautical Research Committee | TIBKAT | 1920/21(1924) - 67.1945(1955)


    Aeronautical Research Council Reports

    Emerald Group Publishing | 1945