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STRESS ANALYSIS

Skin deep (design and test data on stiffeners and stiffened sheets as well as cylindrical structures), by J. S. Newell. Avia-tion, New York, Nov.~Dec. 1935, v. 34, no. 11-12, p. 18-20; 19-20.

t

The Stabllity of a monocoąue in compression (critical loads), by

J.    L. Taylor. London, H.M« Stat. off., 1935.    8 p. diagrs.

(A.R.C. R. & M. no. 1679)

Naturę of the torsional stability of a monocoąue fuselage, by

K.    Sezawa. Journal of the R.A.S., London, May 1933, Mar. 1934, v. 37-38, no. 269, 279, p. 411-22; 268. diagrs., tables.

An Investigation of the stress distribution due to bending and

torąue in Boeing XP-9 semi-monocoąue fuselage, by C.G. Brown. V/ashlngton, U.S. Govt. print. off., 1934.    17 p. diagrs.,

tables. (Air corps Information circular no. 684)

Metal monocoąue construction, by Roy G. Miller. Aviution en-

gineering, New York, Jan. 1933, v. 8, no. 1, p. 10-11, 26.

Formulas for stress analysis of circular rings in a monocoąue

fuselage, by R. A. Miller and K. D. Wooć. Washington, 1933. 22 p. diagrso, illus., tables. (N.A.G.A. Technical notes no.'462) CAbstract Journal of the R.A.S., London, Oct. 1934, p. 348)

Monocoąue fuselage, by W. Nelson. Aviation engineering, New York, Apr. 1932, v. 6, no. 4, p. 11-15, 47.

Longitudinal and transverse shearing stress in monocoąue fuselage of constant or variable cross-sections, by H. W.

Sibert. Washington, U.S. Govt. print. off., 1932.    2 p.

(Air corps information circular no. 675)

PANELS

Measurement of stiffener stresses and effective witiths in stiffened panels, by Holley B. Dickman and J. Robert Fischel. Journal of the aeronautical Sciences, New York, Apr. 1939, v. 6, no. 6, p. 249-54. diagrs., illus., tables.

Stress distribution in reinforcea panels, by Tung-Hua Lin. Journal of the aeronautical Sciences, New York, Nov. 1938, v. 6, no. 1, p. 24-26. diagrso, illus., tables.

Uber den kraftverlauf in 13ngs und quer versteiften schalen, von H. Ebner und H. Kóller. Luftfahrtforschung, MUnchen, Oct. 10, 1938, v. 15, no. 10-11, p» 527-42. illus., tables.