Report of Committee for Year 1930-31: Technical Report by Accidents Investigation Sub-Committee on Accident to Airplane GAAZK at Meopham, Kent, on 21st July, 1930 (R. and M. 1360); Investigation of Possible Cause of Aircraft Fires on Crash, W. G. GLENDINNING; Directional Stability of High Speed Aircraft, W. G. JENNINGS; Quantitative Measurements of Longitudinal Control and Stability of Bristol Fighter When Stalled, with Reference to Stalled Landings, E. T. JONES and R. P. ALSTON; Application of Method of Operators to Calculation of Disturbed Motion of Airplane, L. W. BRYANT and D. H. WILLIAMS; Comparative Handling Tests of Three Bristol Fighter Aircraft with Different Types of Slots, C. E. MAITLAND and J. H. C. WAKE; Stalled Flight Tests on Bristol Fighter Fitted with Auto Control Slots and Interceptors, R. B. ALSTON and Pilots of Aerodynamics Flight; Full Scale Determination of Motions at Stall, of Bristol Fighter Aeroplane with Slot and Aileron Control on Both Planes, K. W. CLARK; Hinge Moments of Balanced and Unbalanced Ailerons on R.A.F. 14 Wing, to Large Angles of Incidence, F. B. BRADFIELD and R. A. FAIRTHORNE; Tests of Various Lateral Controls Fitted to Siskin Aircraft, W. G. JENNINGS; Spinning Experiments on Single Seater Fighter. Part I -- Further Model Experiments, A. S. BATSON and H. B. IRVING, Part II -- Full Scale Spinning Tests, S. B. GATES; Spinning Experiments and Calculations on Model of Fairey IIIF Seaplane with Special Reference to Effect of Floats, Tailplane Modifications, Differential and Floating Ailerons and "Interceptors", H. B. IRVING and A. S. BATSON; Measurements of Accelerations on Aircraft During Manoeuvres, E. FINN and A. E. W. NUTT; Maximum Force on Rudders, F. B. BRADFIELD; Maximum Force on Fin and Rudder of Bristol Fighter, F. B. BRADFIELD and R. A. FAIRTHORNE; Mathematical Investigation of Strength of Wooden Seaplane Hulls of Linton-Hope Type of Construction. (Full Sized Machines -- Third Series), W. C. S. WIGLEY; Stresses in Radially Spoked Wire Wheel under Loads Applied to Rim. Part III -- Simplified Formulae and Curves, A. J. S. PIPPARD and W. E. FRANCIS; Several Cases of Non-Circular Torsion Solved by Analysis and Direct Test, J. ORR; Experiments on Models of Compressed Air Wind Tunnel, R. JONES and A. J. BELL; 5 ft. Open Jet Wind Tunnel, R.A.E., F. B. BRADFIELD; Validity of Large Scale Tests on Open Jet Wind Tunnel; Tests on One-Fifth Scale Bristol Fighter (7.9-ft. Span) in 5-ft. Open Jet Tunnel, W. G. A. PERRING and C. CALLEN; Measurement of Maximum Lift in Closed Tunnels of Different sizes, and in Open Jet Tunnel, F. B. BRADFIELD, K. W. CLARKE and R. A. FAIRTHORNE; Validity of Drag Tests on Large Scale Model in Small Closed Wind Tunnel. Drag of one-fifth Scale Nacelle Installed on Upper Surface of Monoplane, F. B. BRADFIELD and W. G. A. PERRING; Variation of Velocity in Neighborhood of Throat of Constriction in Wind Channel, T E. STANTON; Ventilation of 24-ft Tunnel, B. LOCKSPEISER: Carburetter Fuel Metering Characteristics, W. C. CLOTHIER; Detonation. Mineral Lubricating Oils and Blended Fuels, R. O. KING and H. MOSS; Oxidation Characteristics of Fuel Vapours with Regard to Engine Detonation, E. MARDLES; Limits of Compression Ratio in Diesel Engines, D. R. PYE; Application of Dimensional Relationships to Air Compressors, with Special Reference to Variation of Performance with Inlet Conditions, R. S. CAPON and G. V. BROOKE; Deformation of Single Crystal of Silver, H. J. GOUGH and H. L. COX; Influence of Titanium Tetrachloride on Gas Content and Grain Size of Aluminum and Some Alloys, W. ROSENHAIN. J. D. GROGAN and T. H. SCHOFIELD; Gas Removal and Grain Refinement in Aluminum Alloys. W. ROSENHAIN, J. D. GROGAN and T. H. SCHOFIELD; Protection of Magnesium Alloys Against Corrosion. H. SUTTON and L. F. LE BROCO: Tests on Biplane Fins on Model of R.101 Hull, R. JONES and A. H. BELL; Drag of Flags. R. A. FAIRTHORNE: Full Scale Measurement of Lift and Drag of Large Seaplanes -- Experiments on Blackburn "Iris", L. P. COOMBES and R. K. CUSHING. (See also 1£ 12s 6d)


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    Title :

    Technical Report of Aeronautical Research Committee 1930-31


    Additional title:

    Technical Report Aeronautical Research Committee



    Publication date :

    1932


    Size :

    504 pages


    Remarks:

    Figures, Diagrams, Tables, Charts


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English





    Technical report / Aeronautical Research Committee

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