Report of committee for year 1929-1930: Full Scale Determination of Lateral Resistance Derivatives of Bristol Fighter Airplane; Part III -- Determination of Rate of Roll Derivatives, E. T. JONES; Measurement of Lateral Derivatives on Whirling Arm, L. W. BRYANT and A. S. HALLIDAY; Force and Moment on Oscillating Airfoil, H. GLAUERT; Stability Derivatives of Bristol Fighter, S. S. HALLIDAY; Lateral Stability Calculations for Bristol Fighter Airplane, A. S. HALLIDAY and C. H. BURGE; Simplified Analysis of Stability of Airplanes, W. L. COWLEY and S. W. SKAN; Study of Polynomial Equations, W. L. COWLEY and S. W. SKAN; Some Early Model Experiments on Devices for Improving Lateral Control Near Stall, H. B. IRVING and A. S. BATSON; Lateral Motions of Stalled Bristol Fighter Airplane with Slots upon Upper Wing Tips (Experiments Made in Cambridge University Air Squadron), B. M. JONES, C. E. MAITLAND and R. P. ALSTON; Full Scale Determination of Motion of Avro Airplane When Stalled, K. W. CLARK and W. G. JENNINGS; Experiments on Ape Airplane Fitted with Pilot Planes, S. SCOTT-HALL; Tests On Atlas Fitted with Automatic Slots Connected with Ailerons and Design of Auto-Slots for R.A.F. 28 Section Wing, E. T. JONES; Stalled Flight Tests of Moth Fitted with Auto Control Slots and Interceptors, E. T. JONES, C. E. MAITLAND and W. E. PURDIN; Center of Pressure Travel of Symmetrical Section at Small Incidence, F. B. BRADFIELD; Application of Servo Principle to Aileron Operation, A. S. HARTSHORN; Theoretical Relationship for Wing with Unbalanced Ailerons, A. S. HARTSHORN; Controllability at Low Speeds and Full Scale Measurement of Lift and Drag of Parnall "Peto" Fitted with R.A.F. 15 and R.A.F. 31 Section Wings (Slotted and Unslotted), R. K. CUSHING; Maximum Lift Coefficient of R.A.F. 30 All-Moving Rudder, F. B. BRADFIELD; Rolling and Sideslip Experiments on Model Slotted Biplane of R.A.F. 31 Section, H. B. IRVI NG, A. S. BATSON and A. L. MAIDENS; Spinning of Bristol Fighter Aeroplane, K. V. WRIGHT; High Frequency Fatigue, G. F. JENKIN and G. D. LEHMANN; Behavior of Single Crystals of Zinc Subjected to Alternating Torsional Stresses, H. J. GOUGH and H. L. COX; Behavior of Single Crystal of Antimony subjected to Alternating Torsional Stresses, H. J. GOUGH and H. L. COX; Influence of Oxygen on Corrosion Fatigue, A. M. BINNIE; Elasticity of Pintsch Crystals of Tungsten, S. J. WRIGHT; Properties of Alloys of Aluminum with Thorium and Silicon, J. D. GROGAN and T. H. SCHOFIELD; Mechanical Properties of Pure Magnesium and Certain Magnesium Alloys in Wrought Condition (continued). Mechanical Properties of "Electron" Alloy, H. J. TAPSELL, S. L. ARCHBUTT and J. W. JENKIN; Mechanical Properties of Pure Magnesium and Certain Magnesium Alloys in Wrought Condition (continued), S. L. ARCHBUTT, and J. W. JENKIN; Torsional Vibration of Crankshafts; Beardmore "Tornado" Airship Engine Investigations, B. C. CARTER and N. S. MUIR; Harmonic Analysis of Torque Curves of Single Cylinder Electric Ignition Engine When Throttled to Various Mean Indicated Pressures, N. S. MUIR and A. TERRY; Torsional Vibration of Crankshafts; Description of R.A.E. Mk. III Torsiograph, Staff of Engine Experimental Department; Royal Aircraft Establishment; Performance of Compression Ignition Unit with Reduced Intake and Exhaust Pressures, P. H. STOKES; Experiments on Ignition of Gases by Sudden Compression, R. W. FENNING and F. T. COTTON; Engine Performance with Gaseous Fuels: Part I -- Characteristics and Engine Performance of Gaseous Fuels Obtained from Oil; Part II -- Engine Performance from Kerosene/Oil Gas Mixtures, W. HELMORE; Experiments on Flame Extinction in Gaseous Mixtures, W. HELMORE; Detonation and Lubricating Oil, R. O. KING and H. MOSS; Fuel Flowmeters Designed to Measure Mass Flow, P. S. KERR, with Appendices by D. ROLINSON, R. J. PENN and W. C. COPPER; Wind Tunnel Experiments on Steam Condensing Radiators, R. G. HARRIS, L. E. CAYGILL and R. A. FAIRTHORNE; Determination of Water Resistance of Seaplanes, H. M. GARNER and L. P. COOMBES; Stability of Body Towed by Light Wire, H. GLAUERT; Micromanometer of High Sensitivity, E. OWE R; Airplane as Source of Sound, M. D. HART. (1 pound, 17 shillings, 6 pence)
Technical report of Aeronautical Research Committee, 1929-30
Stability Control, Spinning, Materials, Engines, Etc.
1931
669 pages
Figs., Diagrs., Tables, Plates
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Technical report of aeronautical research committee 1929-30
Engineering Index Backfile | 1931
Technical report / Aeronautical Research Committee
TIBKAT | 1920/21(1924) - 67.1945(1955)
|Technical report of Aeronautical Research Committee 1938
Engineering Index Backfile | 1947
Technical Report of Aeronautical Research Committee 1930-31
Engineering Index Backfile | 1932
Technical report of Aeronautical Research Council
Engineering Index Backfile | 1955