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    On the design of railway wagons for the carriage of perishable foods

    Engineering Index Backfile | 1919

    An investigation of the aerodynamic properties of wing ailerons

    The balancing of ailerons by the Avro patent method / by H. B. Irving, and A. S. Batson
    Irving, H. B. / Batson, Alan S. | SLUB | 1921

    Model experiments on the pitching moment and hinge moment due to elevators of various sizes on B.E.2c tailplane

    Irving, H. B. / Batson, Alan S. | SLUB | 1921

    Report of the Accidents Investigation Sub-Committee on stability terms

    Großbritannien, Aeronatical Research Committee, Accidents Investigation Sub-Committee | SLUB | 1921

    On the modification of the performance of an airscrew due to the propinquity of a plane surface : also experiments with the same model airscrew when mounted behind a model of a power car of airship R.32

    Fage, A. / Howard, R. G. | SLUB | 1921

    Model experiments with variable camber wings

    Harris, R. G. / Bradfield, F. B. | SLUB | 1921

    A comparison of the rates of heat dissipation of an underslung and nose radiator on S.E.5 (S.E.5a and S.E.5b)

    Royal Aircraft Establishment, Aerodynamics Staff | SLUB | 1921

    The effect of the position of the pressure head on a biplane on the speed indication

    Royal Aircraft Establishment, Aerodynamics Staff | SLUB | 1921

    The stability of airships : discussion of the turning trials of the airship R.33

    Simmons, Leonard Frederick George / Nayler, Joseph L. | SLUB | 1921

    Comparative performance of various airscrews for S.E.5a with Wolseley Viper engine

    Stevens, H. L. / Lynam, E. J. H. | SLUB | 1921

    Note on recording instrument for kite balloon

    Smith, G. L. | SLUB | 1921

    Cushioning effect on aeroplanes close to the ground

    Cowley, William L. / Lock, C. N. H. | SLUB | 1921

    German aerofoil tests

    Lang, E. D. | SLUB | 1921

    Experiments on the effect of fairing the nose of an S.E.5 fuselage

    Royal Aircraft Establishment, Aerodynamics Staff | SLUB | 1921

    Comparison of the flying qualities of single and twin engined aeroplanes

    Hill, R. M. | SLUB | 1921

    The manœuvres of getting off and landing

    Hill, R. M. | SLUB | 1921

    The effect of the lag of the downwash on the longitudinal stability of an aeroplane and on the rotary derivative M q

    Cowley, William L. / Glauert, Hermann | SLUB | 1921

    Note relating to two oscillation methods in use for determining rotary derivatives of models

    Simmons, Leonard Frederick George | SLUB | 1921

    Some tests on navigation instruments during a flight of rigid airship H.M.A. R.33

    Bygrave, L. C. | SLUB | 1921

    Note on the inverted loop

    Pippard, Alfred John Sutton | SLUB | 1921

    The canonical forms of the equations of motion of an aeroplane in still and gusty air

    Bryan, George H. | SLUB | 1921

    The acoustics of moving sources with application to airscrews

    Bryan, George H. / Lamb, H. | SLUB | 1921

    Preliminary note on the effect of stagger and décalage on the auto-rotation of a R.A.F.15 biplane

    Irving, H. B. / Batson, Alan S. | SLUB | 1921

    The effect of a proposed passenger car on the resistance of airship R.33

    Jones, R. / Bell, A. H. | SLUB | 1921

    Tests of four aerofoils suitable for airscrew design

    Searle, N. S. / Peatfield, I. L. | SLUB | 1921

    The influence of military and civil requirements on the flying qualities of aeroplanes

    Hill, R. M. | SLUB | 1921

    The application of the results of experiments on model airships to full scale turning

    Jones, R. | SLUB | 1921

    An analysis of the conditions governing the requisite strength of aeroplane structures

    Pippard, Alfred John Sutton | SLUB | 1921

    Forced vibrations in aeroplane instruments

    Wimperis, H. E. | SLUB | 1921

    Note on landing in fog

    Lindemann, F. A. | SLUB | 1921

    Experiments on an S.E.5A aeroplane with modified control surfaces

    Royal Aircraft Establishment, Aerodynamics Staff | SLUB | 1921

    The distance required to take off an aeroplane

    MacKinnon Wood, R. / Bradfield, F. B. | SLUB | 1921

    Torsional stresses in the fuselage of an aeroplane

    Pippard, Alfred John Sutton / Douglas, W. D. | SLUB | 1921

    On the determination of the stresses in braced frameworks

    The effects of axial loading, flexure and torsion upon a framework of uniform rectangular cross-section
    Southwell, Richard V. | SLUB | 1921

    Tests on a model of the dreadnought Postal Type monoplane

    Ower, Ernest | SLUB | 1921

    Pressure distribution on wing with fixed balanced aileron (square horn type)

    Batson, Alan S. | SLUB | 1921

    A note on the method of estimating from observations of total head, the total thrust of an airscrew

    Fage, A. | SLUB | 1921

    Experiments with full sized machines : second series

    Baker, G. S. / Keary, E. M. | SLUB | 1921

    Aerofoil theory

    Glauert, Hermann | SLUB | 1921

    Experiments on the direct effect of adding a spinner to S.E.5

    Royal Aircraft Establishment, Aerodynamics Staff | SLUB | 1921

    An analysis of the steady two-dimensional flow of an incompressible viscous fluid

    Cowley, William L. / Levy, H. | SLUB | 1921

    The sounds of aeroplanes

    SLUB | 1921

    Summary of the present state of knowledge with regard to stability and control of aeroplanes

    Glauert, Hermann | SLUB | 1921

    Lift and drag of S.E.5 aeroplanes : comparison of full scale and model results

    Glauert, Hermann / Peatfield, I. L. | SLUB | 1921

    An analysis of the conditions governing the requisite strength of aeroplane structures

    Pippard, Alfred John Sutton | TIBKAT | 1921

    Aerofoil theory

    Glauert, Hermann | TIBKAT | 1921

    Torsional stresses in the fuselage of an aeroplane

    Pippard, Alfred John Sutton / Douglas, W. D. | TIBKAT | 1921

    Acceleration derivatives in the case of a body moving in an ideal fluid

    Jones, R. | SLUB | 1922

    Experiments on complete models of six aeroplanes

    Relf, E. F. | SLUB | 1922

    An investigation of the aerodynamic properties of wing ailerons

    The effect of yaw on the balance of ailerons of the "horn" type / by H. B. Irving, and A. S. Batson
    Irving, H. B. / Batson, Alan S. / Hill, G. T. R. | SLUB | 1922

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