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STRESS ANALYSIS

Relaxation methods applied to a spor of varying section, deflect-ed by transverse loading combined with end thrust or tension, by K.N.E. Braafield, R.J. Atkinson and F.R.S. Southwell. London, H.M. Stat. off., 1937.    33 p. diagrs., illus., table.

(A.R.C. R. & M. no. 1820)

Ebene blechwandtrUger mit nichtparallelen holmen, von C. Schmieden. Luftfahrtforschung, MUnchen und Berlin, Mov. 20, 1936, v. 13, no. 11, p. 391-93. diagrs., illus. (Abstract Aircraft en-gineering, London, Feb. 1957, v. 9, no. 96, p. 55)

Knickbiegung von flugzeugholmen bei linear ver&nderlicher

langskrcft, von C. Schmieden. Luftfahrtforschung, MUnchen und Berlin, June 20, 1936, v. 13, no. 6, p. 178-80. diagr., tables.

Influencia de la torsión de los largueros en el calculo de un ala, por F. 01ivencia. Revista de aeronautica, Madrid, June 1936, v. 5, no. 51, p. 307-10. diagrs.

Precise moment eduations, by A.W. Burgess. Aero digest, New York, Dec. 1935, v. 27, no. 6, p. 26, 30, 52. illus., tables.

A Nev; method of stressing wooden spars, by W. Prager. Flight, London, July 25, 1935, p. 102a-f. diagrs., illus.

The Strength of aeroplane v;ing spars with end loads varying in any one bay, by J. Morris. Journal of the R.A.S., London,

June 1934, v. 38, no. 282, p. 515-18.

The Effect of the ribs on the stresses in the spars of a two-

spar wing subjecteć to the most generał type of loading, by D. Williams and K. Roxbee Cox. London, H.M. Stat. off.,

1933.    11 p. diagrs. (A.R.C. R. & M. no. 1538)

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Flexural and shear deflection of metal spars, by I.J. Gerard and H. Boden. London, H.M. Stat. off., 1933.    11 p. diagrs.,

illus., tables. (A.R.C. R. & M. no. 1567) (A_b_str.ac.ts L^łAerotecnica, Roma, Apr. 1255, v. 15, no. 4, p. 428 and Mechanical engineering, New York, Sep. 1936, v. 58, p. 592)

Zur berechnung auf knickbiegung beanspruchter flugzeugholme, von A. Teichmar.n. Z.F.M., Berlin, Sep. 14, 1932, v. 23, no. 17, p. 511-19.

Berechnungstabełlen der knicklast Uber den Eulerschen wert fUr zweifelarige tragfl&chenholme der flugzeuge, von P. Orszag.

Der Bauingenieur, Berlin, Sep. 9, 1932, v. 13, no. 37-38, p. 480-81.

Late developments in airpiane stress-analysis method and their effect on airplane strućtures, by Richard C. Gazley.

S.A.E. Journal, New York, Sep. 1932, v. 31, no. 3, p. 345-55. illus.