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STRESSED SKIN, SHELLS

Stressed-skin construction. (distribution of loads on. stringers and transverse rings in a monocoąue fuselage), by W. Tye. Flight, London, Aug. 26, 1937, v. 32, no. 1496, p. 212a-e. illus.

Stress distribution in stiffenea panels under compression, by E. E. Sechler. Journal of the aeronautical Sciences,

New York, June 1937, v. 4, no. 8, p. 320-23. diagrs., illus.

Tests of Steel columns, thin cylindrical shells, laced cnannels, angles, by Wilbur M. Wilson. Bulletin of the university of Illinois engineering experiraental station, Urbana, 111., Apr. 1937, no. 292, p. 5-39. diagrs., illus., tables.

Einfluss der nietteilung auf die druckfestigkeit versteifter

schalen aus duraluminium, von A. Kromm. Luftfahrtforschung, MUnchen, Mar. 20, 1957, v. 14, no. 3, p. 116-20. diagrs., illus., tables.

Uber die stabilitat orthotroper elliptischer zylinderschalen bei

reiner biegung, von 0. S. Heck. Luftfahrtforschung, MUnchen, Mar. 30, 1937, v. 14, no. 3, p. 137-47. diagrs., illus., tables.

Uber die stabilitat dUnnwandiger hohlzylinder und rechteckiger

bleche oberhalb der proportionalit&tsgrenze, von W. Kaufmann. Der Stahlbau, Berlin, Jan. 1, 1937, no. 1, p. 1-4. diagrs.

The Strength of Shell bodies - theory and practice, by H. Ebner. Washington, 1937.    51 p. diagrs., illus. (N.A.C.A. Tech-

nical memoranduras no. 838) (From Luftfahrtforschung, MUnchen und Berlin, Mar. 20, 1937, v. 14, no. 3, p. 93-115)    (Abstraćt

Journal of the R.A.S., London, Jan. 1938, p. 100)

The Stress distribution in Shell bodies and wings as an eąuilibrium problem, by H. Wagner. Washington, 1937.    29 p. (N.A.C.A.

Technical memoranćums no. 817) (From Luftfahrtforschung, MUnchen, Sep. 20, 1936, v. 13, no. 9, p. 281-92) ¹

Application of stress in thin-wallea cylindrical shells, by H.

Wagner and H. Simon. Air.craft engineering, London, Nov. 1936, p. 319-20.

Stresses in the rings of stressed skin fuselages due to vertical shears, by G. F. Wallace. Flight, London, Oct. 1, 1936, v. 29, p. 17-19. illus. (Aiso Journal of the R.A.S.,

London, Apr. 1936, v. 40, no. 304, p. 304-12)    (Abstrąc.t

L^łAerotecnica, Roma, Feb. 1937, v. 17, p. 142)

Stress and strain in a thin elliptic cylinder under internal pres-sure, by W- S. Brown. Engineer, London, Aug. 28, 1936, v. 162, p. 201-02. diagrs., illus.