1–20 von 63 Ergebnissen
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    Crinkling strength and bending strength of round aircraft tubing

    Osgood, W.R. | Engineering Index Backfile | 1938
    strength and ratio of diameter to thickness; empirical formulas given relating to these qualities. ...
    Verlag: National Advisory Committee for Aeronautics

      Crinkling strength and bending strength of round aircraft tubing

      Osgood, W.R. | Engineering Index Backfile | 1938
      strength and ratio of diameter to thickness; empirical formulas are given relating these quantities. ...
      Verlag: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Strength calculations on airplanes

    Baumann, A. | Engineering Index Backfile | 1925
    Verlag: National Advisory Committee for Aeronautics

    Strength of welded aircraft joints

    Brueggeman, W.C. | Engineering Index Backfile | 1937
    Verlag: National Advisory Committee for Aeronautics

      Strength of welded aircraft joints

      Brueggeman, W.C. | Engineering Index Backfile | 1937
      Verlag: National Advisory Committee for Aeronautics

      Strength of welded aircraft joints

      Brueggeman, W.C. | Engineering Index Backfile | 1937
      Verlag: National Advisory Committee for Aeronautics

    The torsional strength of wings

    Burgess, C.P. | Engineering Index Backfile | 1929
    bottom of wing greatly increases torsional strength; analytical procedure for finding contribution of drag bracing to torsional strength and ...
    Verlag: National Advisory Committee for Aeronautics

    Torsional strength of stiffened D-tubes

    Kavanaugh, E.S. / Drinkwater, W.D. | Engineering Index Backfile | 1951
    Torsional strength of stiffened D-tubes. ...
    Verlag: National Advisory Committee for Aeronautics

    Compressive strength of tapered airplane struts

    Lewe, Viktor | Engineering Index Backfile | 1923
    Methods for ascertaining value of n in Euler's simplified formula for compressive strength of tapered airplane struts, by estimating from ...
    Verlag: National Advisory Committee for Aeronautics

    Development of rules governing strength of airplanes

    Kuessner, H.G. / Thalau, K. | Engineering Index Backfile | 1933
    Verlag: National Advisory Committee for Aeronautics

      Development of rules governing strength of airplanes

      Kuessner, H.G. / Thalau, K. | Engineering Index Backfile | 1933
      Verlag: National Advisory Committee for Aeronautics

    On the strength of box-type fuselages

    Mathar, J. | Engineering Index Backfile | 1929
    Verlag: National Advisory Committee for Aeronautics

    Strength of shell and tubular spar wings

    Ebner, H. | Engineering Index Backfile | 1940
    Verlag: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    The air propeller, its strength and correct shape

    Dietsius, H. | Engineering Index Backfile | 1923
    Verlag: National Advisory Committee for Aeronautics

    Biaxial fatigue strength of 24S-T aluminum alloy

    Marin, J. / Shelson, W. | Engineering Index Backfile | 1949
    Biaxial Fatigue Strength of 24S-T Aluminum Alloy. ...
    Verlag: National Advisory Committee for Aeronautics

    Strength of plane web systems in incomplete diagonal tension

    Kuhn, P. / Chiarito, P.T. | Engineering Index Backfile | 1942
    Strength of plane web systems in incomplete diagonal tension. (Advance Restricted Report Aug 1942) ...
    Verlag: National Advisory Committee for Aeronautics

    Strength of welded joints in tubular members for aircraft

    Whitteman, H.L. / Brueggeman, W.C. | Engineering Index Backfile | 1930
    Investigation on strength, weight, and cost of number of types of welded joints; 40 joints were welded under procedure specifications and ...
    Verlag: National Advisory Committee for Aeronautics

    Some strength tests of stiffened curved sheets loaded in shear

    Chiarito, P.T. | Engineering Index Backfile | 1944
    Verlag: National Advisory Committee for Aeronautics

    Strength tests of thin-wall truncated cones of circular section

    Lundquist, E.E. / Schuette, E.H. | Engineering Index Backfile | 1942
    Strength Tests of Thin-Wall Truncated Cones of Circular Section. (Advance Restricted Report) ...
    Verlag: National Advisory Committee for Aeronautics

    Mercerization of cotton for strength with special reference to aircraft cloth

    Wilkie, J.B. | Engineering Index Backfile | 1933
    Bureau cotton mill; results show improvement in strength of 100%. ...
    Verlag: National Advisory Committee for Aeronautics

    On shear strength of skin-stiffener panels with inspection cut-outs

    Kuhn, P. / Diskin, S.H. | Engineering Index Backfile | 1945
    On shear strength of skin-stiffener panels with inspection cut-outs. (Advance Restricted Report L5C01a Mar 1945) ...
    Verlag: National Advisory Committee for Aeronautics

    Analysis of ultimate strength and optimum proportions of multiweb wing structures

    Rosen, B.W. | Engineering Index Backfile | 1956
    Analysis of Ultimate Strength and Optimum Proportions of Multiweb Wing Structures. ...
    Verlag: National Advisory Committee for Aeronautics

    Data on compressive strength of skin-stringer panels of various materials

    Dow, N.F. / Hickman, W.A. / Rosen, B.W. | Engineering Index Backfile | 1954
    Data on Compressive Strength of Skin-Stringer Panels of Various Materials. ...
    Verlag: National Advisory Committee for Aeronautics

    Tensile-strength investigation of cast-iron piston rings of various strengths

    Bisson, E.E. / Kessler, H.D. | Engineering Index Backfile | 1945
    Verlag: National Advisory Committee for Aeronautics