5340783145
198
STRESS ANALYSIS
Precise moment eąuations, by A.W. Burgess. Aero digest, New York, Dec. 1935, v. 27, no. 6, p. 28, 30, 52. illus., tables.
Sforzi interni indotti nelle cellule dei velicoli da errata rego-lazione e loro conseguenze, di Angelo Vallerani. LfAerotec-nica, Roma, July-Aug. 1935, v. 15, no. 7-8, p. 800-15. diagr. illus., tables.
Analysis of 2-spar cantilever wings with special reference to torsion and load transference, by Paul Kuhn. Washington,
U.S. Govt. print. off., 1935. 22 p. (N.A.C.A. Report
no. 508)
Exemples de remplacenent dłune diagonale dans le treillis du fuselage par un systeme de barres, par W. Billewicz et A. Grzedzielski. Warsaw, Instytut Badań technicznych lotnictwa, Sprawozdania, 1935, v. 8, no. 2, p. 20-48. diagrs., tables. (in polish and french)
Stress analysis of a two-spar tapereć v/ing under torsion, by G. Elenevsky. Moscow, Scientific technicsl department of the Supreme council of national economy, 1935. (C.A.H.I.
Transactions no. 208)
Strength calculations for a tubular single-spar cantilever wing, by F. Duncanson. Flight, Lordon, Sep. 27, 1934, v. 27, no. 1344, p. 1002a-d. diagrs., tables.
Analyzing wing beams by means of polar diagrams, by R.H. Schwarz. Aero digest, Nev; York, June-July 1934, v. 24-25, p. 38-41; 18-21.
Sulla torsione delle ali a sbalzo, di P. Cicala. LfAerotecnica, Roma, July 1934, v. 14, no. 7, p. 827-53. diagrs.
Strutture alari a due longaroni eon centine, di C. Minelli.
LłAerotecnica, Roma, May 1234, v. 12, no. 5, p. 493-531.
Continuous beam design by successive influence lines, by I.
Duberstein. Engineering news-record, New York, Apr. 12, 1934, v. 112, no. 15, p. 471-73.
Le Calcul des ailes k revetement rigiae, par Paul Bodet. LłAero-phile, Paris, Nov.-Dec. 1933, no. 11-12, p. 336-58; 364-65. diagrs., illus.
Determinación^de las cargas en una celula de aeroplano. Revista de aeronautica, Madrid, Oct. 1933, v. 2, no. 19, p. 545-53. diagrs., illus.
Sul calcolo delle ali dei velivoli, di R. Yerduzio. LfAerotecnica Roma, Mar. 1933, v. 13, no. 5, p. 178-84.
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