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W IN GS

Entwurf und berechnung von flugzeugen. Vol. I - TragflUgel freitragender tiefdecker, von G. Otto. Berlin, Verlag Volckmann nachf., 1937.    88 p. illus.

The Stress distribution in shell bodies and wings as an eąuili-brium problem, by H. Wagner. Washington, 1937.    29 p.

(N.A.C.A. Technical memor&ndums no. 817) (Front Luftfahrt-forschung. MUnchen und Berlin, Sep. 20, 1936, v. 13, no. 9, p. 281-92)

A Method of figuring shear and torsion in multispar wings, by

F. Nagel. Journal of the aeronautical Sciences, New York, Nov. 1936, v. 4, no. 1, p. 8-9.- diagrs., illus.

Sistemi elastici eon infiniti legami sovrabbondanti, di Carlo Minelli. L^rAerotecnica, Roma, Nov. 1936, v. 16, no. 11, p. 802-19. diagrs.

Influencia de la torsion de los largueros en el calculo de un ala, por F. Olivencia. Revista de aeronautica, Madrid, June 1956, v. 5, no. 51, p. 307-10. diagrs.

Stressing of multi-spar wings, by Harold N. Horne. Flight,

London, May 28, 1936, v. 29, no. 1431, p. 576c-f. diagrs., tables.

The Stressing of monoplane wings, by H.N. Horne. Flight,

London, Mar. 26, Apr. 30, 1936, v. 29, no. 1422,^1427, p. 17-19; 27-29. diagrs., illus., tables.

Two-spar cantilever wings, by B. B. Walker. Flight, London,

Dec. 26, 1935, Jan. 23, 1936, v. 28-29, no. 1409, 1413, p. 41-42, 84C-89.

The Distribution of stress in monocoąue wings, by H. F. Winny. London, H.M. Stat. off., 1936.    12 p. diagrs. (A.R.C.

R. & M. no. 1756) (Review Flight, London, Sep. 30, 1937,

p. 20)    •'    *

A General method of calculating the effect of axial constraint on torsions of different forms of two-spar, skin covered wir.gs, by A.E. Russell. London, H.M. Stat. off., 1936.

16 p. diagrs., tables. (A.R.C. R. & M. no. 1757) (Abstrakt L^fAerotecnica, Roma, Dec. 1937, p. 1082)

On the stressing of aeroplane wings due to symmetrical gusts,

by L.W. Eryant and I.M.W. Jones. London, Ii.M* Stat. off.. 1936. 19 p. diagrs., tables. (A.R.C. R. & M. no. 1690)

Remarks on the elastic axis of Shell wings, by Paul Kuhn. Washington, 1936.    10 p. diagrs. (N.A.C.A. Technical notes

no. 562) (Abstraćt Journal of the R.A.S., London, Sep. 1936, p. 736)~