5340783151

WINGS

Investigation of wing stresses. Experiments on fraraeworks, by L.N.G. Filon. Aeronautics, London, Sep. 18, 1919, v. 17, no. 3Q9, p. 281-83.

Tragliiehendurchbiegimg und stoffbeanspruchung, von A. Proll.

ZVF•M., MUnchen, June 28, 1919, v. 10, no. 11-12, p. 121-24

Incidence wires in the strength calculations of wing structures by John Case. Aeronautics, London, Dec. 4, 18, 25, 1918, v. 15, no. 268, 270-71, p. 516-17; 566-70; 602-07. diagrs.

Course in aerodynamics and airplane design. Part 2, section 12. Wing-strućturę analysis for biplanes, by Alexander Klemin and T.H. Huff. Aviation and aeronautical engineering,

New York, Aug. 1, 1917, v. 3, no. 1, p. 33-36. diagrs.

Course in aerodynamics and airplane design. Part 2, section 11. Wing-structure analysis for biplanes, by Alexander Klemin and T.H. Huff. Aviation and aeronautical engineering, New York, July 15, 1917, v. 2, no. 12, p. 559-61. diagrs.

Graphieal treatment of elastic ribs, by C. S. Whitney. Cornell civil engineer, Ithaca, New York, Jan. 1916, v. 24, no. 4, p. 144-52. illus.

Wing data and analysis for a staggered biplane, by A.F. Zahm.

Journal of the Franklin institute, Philadelphia, Pa., Dec. 1914, no. 57203B, p. 663-79. diagrs., illus., tables.

Strength of wings of aeroplanes (a study of the stresses, etc.) Engineering, London, Nov. 15, 1912, v. 94, p. 683-84.

Stresses in wings, the R.A.F. method of estimating. Flight, London, Oct. 18, 1912, v. 5, no. 49, p. 1146-49. illus.

Liniting stresses in wings, by B.G. Cooper. Flight, London,

May 25, 1912, v. 4, no. 21, p. 479.

Head resistance and wing stresses. Flight, London, Apr. 6-13, 1912, v. 4, p. 303-305; 327-28.

Aeroplane wing stresses, by Mervyn O^fGorraan. Flight, London, Apr. 27, 1912, v. 4, no. 17, p. 369.

The Stresses on monoplane wings. Engineering, London, Jan. 12, 1912, v. 93, p. 53-54. (Also Aeronautics, London, May 1912 v. 5, no. 51, p. 136)

GENERAL

The Strućturę significance of stress, by Bruce Johnston. Civil engineering, New York, May 1939, v. 9, no. 5, p. 291-94.