5340783170

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STKESS ANALYSIS    I

Stresses in a stiff jointed polygonal frame under a system of

parallel loads. Parts I-II, by A.J. Sutton Pipparu. London,

H. M. Stat. off., 1922, 1924.    14 p. diagrs., tables.

(A.R.C. R. & M. no. 820, 912)    ‘    i

Calculations for a single-strut biplane with referenoo to the    I

tensions in the :ving bracing, by 0. Blumenthal. Washington, 1923.    28 p. diagrs., tables. (N.A.C.A. Technical notes

no. 143)    (Prora    Technische berichte,    Charlottenburg, 1918,    |

v. 3, no.    5^    I

Compressive strength of taperea airpiane struts. Euler^łs simplified; formula, by Victor Lewe. Washington, 1923.    8 p. illus.    ;

(N.A.C.A. Technieal notes no. 171) (Frora Technische berichte, » Ch&rlottenburg, 1918, v. 3, no. 7)    I

The Distributior. of load among the snars in multi-spar eonstruc-tion of airplane wings, by J. S. Newell. Washington, U. S.

Govt. print. off., 1923.    10 p. iilus. (Air service Informa

tion circular no. 394)

The Effect of eccentricities on stresses in airplane spars, by A.S. TJiles and R. A. Miller. Washington, IJ.S. Govt. print. off., 1923.    10 p. diagrs. (Air service Information circular

no. 438)

Analysis of stresses in german airplanes, by Wilhelm Hoff. 'Washington, U.3. Govt. print. off., 1922.    52 p. illus. (N.A.C.

Report no. 143)

Internal stresses in laminated construction, by A. L. Heim, A. C. Knauss and Louis Seutter. Washington, U.S. Govt. print. off. 1922.    56 p. illus. (N.A.C.A. Report no. 145)

A

o

y

Notes on the design of latticed columns subject to lateral loads, by Charles J. McCarthy. Washington. 1922.    18 p. diagrs.

(N.A.C.A. Technical notes no. 98)

On a raethod for the direct design of framed structures having

redundant bracing, by A.-J. Sutton Pippard. London, H.M. ^tat. off., 1922.    11 p. (A.R.C. R. Cc M. no. 795)

i

On the determination of the stresses in braceti frameworks. Part I: The Effects of axial lo&ding, flexure and torsion upon a framev:ork of uniform rectanguiar cross-soction. Part II: The Effect of shear upon a framerork of uniform rectanguiar cross-section. Part III: The Effect of axial loading, torsion flexure and shear upon a braced tubę of any uniform eross-section, by R.V. Southyrell. London, H.M. Stat. off., 1321-1922.    47 p. diagrs. (A.R.C. K. & M. no. 737, 790, 791)

The Reduction of the effective value of Young*s modulus in

flexible compression rnembers, by A. J. Sutton Pippard. London, H.M. Stat. off., 1922.    8 p. diagrs. (A.R.C. R. Cc M.

no. 792)

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