5340783059

STRESS ANALYSIS

Charts for checking the stability of compression members in trusses as of fuselage or wing spars, by K. Borkmann. Washington,

1936.    21 p. diagrs., maps. (N.A.C.A. Technical memoranciums

no. 300) (From Luftfahrtforschung, MUnchen und Berlin, Jan. 20 1936, v. 13, no. 1, p. 1-9)

The Distribution of stress in monocoąue v/ings, by H. F. Winny. London, H. M. Stat. off., 1936.    12 p. charts. (A.R.C. R. & M.

no. 1756)

The Forces and moments on airpiane engine mounts, by Philip Donely. Washington, 1936.    18 p. bibliog., diagr., illus. (N.A.C.A.

Technical notes no. 587) (Abstracts Journal of the R.A.S., London, Apr. 1937, p. 330 and Airsraft engineering, London,

May 1937, p. 141)

Further problems in the theory and design of structures, by E. 8. Andrews. London, Chapman, 1336.    236 p. illus.

Fuselage analysis, by D. R. Adams. (In his Practical aircraft stress analysis. London, Sir Isaac Pitman and sons, ltd.;

New York, Pitman publishing Corporation, 1936. p. 31-77. diagrs., illus., tables)

A General method of calculating the effect of axial constraint on torsions of different forms of two-spar, skin covered wings, by A. E. Russell. London, II. M. Stat. off., 1936.    16 p.

diagrs., tables. (A.K.C. R. & M. no. 1757) (Abstract L^fAero-tecnica, Roma, Dec. 1937, p. 1082)

Graphost&tik, von E. Trefftz. Leipzig und Berlin, B.G.

(In Teubners mathematische leitfaeden. Teubner, 1936.    90 p.)

New York, (Aiso De , p. 57-39) v. 7, no.

Influence lines by moment distribution, by F. Kruys.

Engineering library, 1936.    7 p. illus., tables.

Ingenieur, Den Haag, Mar. 13, 1936, v. 51, no. II (Abs tract Civil engineering, ?Jev; York, Junt* 1937, p. 4315“

A Manuał of photo-clasticity for engineers, by L.N.C. Filon. Nevv York, MacMillan and company, 1936.    140 p. charts, diagrs.,

illus.

The Method of successive increments and Its application tc problems of rigid frame structures, by H. Yu. Wuchang, China, National Wuhan university press, 1936.    77 p. diagrs., tables.

(Rcyiew Engineering, London, Jan. 21, 1938, v. 145, no. 3758,

p. 79)

Methods and formulas for calculating the strength of piąte and

shell constructions as used in airpiane design, by 0.3. Heck and H. Ebner. 'Washington, 1936.    40 p. diagrs. (N.A.C.A.

Technical memoranóums no. 785) (From Luftfahrtforschung, MUnchen und Berlin, Feb. 6, 1335, v. 11, no. 8, p. 211-22)