5340783139

16

STRESS ANALYSIS

Strength of rectangular fiat plates under edge compression, by

Louis Schuman and Goldie Back. V/ashington, U.S. Govt. print. ofi., 1930.    24 p. diagrs., illus., tables. (N.A.C.A.

Report no. 356)

The Stresses in a radially spoked wire Wheel under loads applied to the rim, by A.J. Sutton Pippard and W.E. Francis. London, IM4. Stat. off., 1930.    43 p. diagrs., illus., tables.

(A.R.C. R. & M. no. 1302) (Aiso Philosophlcal magazine and Journal of science, London, Feb. 1931, ser. 6, v. 11, no. 69, p. 233-81)

The Torsion of members having sections comraon in aircraft con-struction, by George W. Trayer and H.W. March. Washington, U.S. Govt. print. off., 1930.    48 p. diagrs. (N.A.C.A.

Report no. 334)    •.

* • •

• *. *»

A

Airplane stress analysis; an introductóry treatise, by Alexanaer Klemin with the collaboration of George F. Titterton. New York, The Ronald press company, 1929.    277 p. diagrs.,

• illus.

The Analysis of aircraft strućtures as space framev/orks. Method based on the forces in the longitudinal members, by Herbert Wagner. Washington, 1929.    35 p. illus. (N.A.C.A. Tech-

nical memorandums no. 522) (From Z.F.M., MUnchen and Berlin, Aug. 14, 1928)

Der Durchlaufende trager, von A. Kleinlogel und G. Sigmann.

Berlin, V/ilhelm Ernst und sohn, 1929.    184 p. diagrs.,

illus.

Measurement of landing loads, by E.T. Jones. London, H.M. Stat.

off., 1929.    8 p. diagrs., illus., tables. (A.R.C. R. & M.

no. 1246) (Abstract L*Aerotecnica, Roma, Jan.-Feb. 1330, v. 10, no. 1-2, p. 78)

On the strength of box-type fuselages, by J. Mathar. Washington, 1929.    11 p. illus. (N.A.C.A. Technical memorandums

no. 511) (From Jahrbuch der W.G.L., Berlin, 1928)

Precise formulas for restrainea beam with axial load of com-

presoion, and with one restraining moment known. Washington, U.S. Govt. print. off., 1929.    3 p. diagrs., tables. (Air

corps information circular no. 624)

Remarks on airplane struts and girders under compressive and bend-ing stresses, by Herbert Wagner. Washington, 1929.    26 p.

diagrs., tables. (N.A.C.A. Technical memorandums no. 500) (From 2.F.M., MUnchen und Berlin, June 14, 1928, v. 19, no. 11 p. 241-47)