5340783155

207

GENERAL

EUf-ine mounting stresses, by R. Roger. Flight, London, May 27, 1932, v. 24, no. 1218-22, p. 468e-g, S76e-g.

II Calcolo di robustezza degli aeroplani, di C. pallavicino.

L^fAla d^fItalia, Milano, July 1931, v. 10, no. 7, p. 529-31. diagrs.

Aufgaben der luftfahrzeug-statik, von Karl Thalau. Z.F.M.,

Berlin, Apr. 28, 1931, v. 22, no. 8, p. 229-41. illus.

Beitrag zur lbsung des ebenen spannungproblems, von E. Kohl.

Z.A.M.M., Berlin, Apr. 1930, v. 10, no. 2, p. 141-60. illus.

Sulle tensioni e sulle deformazioni dl particolari strutture spaziali ad aste eon due cerniere, di Carlo Minelli..

L^fAerotecnica, Roma, Mar. 1930, v. 10, no. 3, p. 131-48. illus.

Criteria for the structural strength of airplanes, by A. S.

Niles. S.A.E. Journal, New York, Feb. 1930, v. 26, no. 2, p. 226-34.

Stress analysis of fittings, by L.F. Engelhardt. Aviation

engineering, New York, Jan. 1930, v. 3, no. 1, p. 11-14.

One hunćred fifty years¹ advance in structural analysis, by

H.M. Westergaard. Proceedings of the A.S.C.E., New York, Apr., Oct. 1928, Aug. 1929, v. 54, 55, p. 993-1007;

2383-86; 1565-67.

Applications of advanced methods to airplane structural analysis, by Michael Watter. Aero digest, New York, June 1929, v. 14, no. 6, p. 102-10. (Also Transactions of the A.S.M.E., New York, 1929, v. 51, pt. 1, p. 97-106.)

Stress analysis of commercial aireraft, by A* Klemin and G.F. Titterton. Aviation, New York, Mar. 12-26, Apr. 9-28,

June 11-18, July 2, 1928, v. 24-25, no. 11-13, 15-22,

24-25; 1, p. 632-33; 654-60; 29, 51-54. illus.

Report of Joint committee on stresses in structural steel. Proceedings of the A.S.C.E., New York, Mar. 1927, v. 53, p. 139-40.

Sollecitazioni nella struttura di un aeromobile, di Carlo Ferrari. L^fAerotecnica, Roma, Aug.-Sep. 1926, v. 6, no. 5, p. 335-51.

Experimental stress analysis. Flight, London, Jan. 14, 1926, v. 18, no. 2, p. 22.