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Volume 41 - December 1937

Contents

Page 3 of 7

Abstract

  • Abstracts from the Scientific and Technical Press

  • Published online by Cambridge University Press:
    28 July 2016, pp. 1144-1161
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  • Abstracts of Patent Specifications

  • Published online by Cambridge University Press:
    28 July 2016, pp. 51-63
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  • Abstracts and Notices from the Scientific and Technical Press

  • Published online by Cambridge University Press:
    28 July 2016, pp. 401-413
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Research Article

  • The Part Played by Skin Friction in Aeronautics

  • F. W. Lanchester
  • Published online by Cambridge University Press:
    28 July 2016, pp. 322-323

  • In Part V of my recent paper, when discussing and tabulating the conditions that obtain at low Reynolds numbers (more especially as concerns the dynamics of flight of the model depicted in Fig. 14), the data shown in Table IX and plotted in Fig. 15 need correction. It appears that in the tabulation an incorrect constant was taken. Furthermore, the distinction which exists at low Reynolds numbers between data secured in the wind channel, in which, generally speaking, wind velocity is constant, and the data relating to a glider in free flight in which W is constant, was not sufficiently explained.

Abstract

  • Abstracts of Patent Specifications

  • Published online by Cambridge University Press:
    28 July 2016, pp. 845-860
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Other

Abstract

  • Abstracts and Notices from the Scientific and Technical Press

  • Published online by Cambridge University Press:
    28 July 2016, pp. 493-506
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Research Article

  • Pin-Jointed Struts

  • L. H. Sumanadasa
  • Published online by Cambridge University Press:
    28 July 2016, pp. 1162-1164

  • Simplified method of solution of the equation,

    1

    • where p = the permissible stress.

    • py = proof stress.

    • d = external diameter of strut.

    • k = radius of gyration.

    • l = length of strut.

    • δ = eccentricity.

    • E = Young's modulus of elasticity.

    This method is mainly developed in order to reduce the time taken to work out a series of curves of permissible stress against (l/k). The graphical methods have so far been elaborate and no definite accuracy can be maintained.

Reviews

Abstract

  • Abstracts of Patent Specifications

  • Published online by Cambridge University Press:
    28 July 2016, pp. 507-518
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Reviews

Abstract

  • Abstracts and Notices from the Scientific and Technical Press

  • Published online by Cambridge University Press:
    28 July 2016, pp. 612-628
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  • Abstracts and Notices * from the Scientific and Technical Press

  • Published online by Cambridge University Press:
    28 July 2016, pp. 324-336
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Reviews

Page 3 of 7