作成：滝 敏美

2011年9月24日

2011年9月24日

「航空機構造解析の基本」を作成するために，多くの文献を調べました．集めた文献の中には，一般的には入手が困難なものがあります．これらの文献をホームページで公開することはしませんが，入手したい方があれば個人的にお送りすることができますので，連絡してください．pdfファイルでお送りします．

メールのあて先は滝 敏美です．

J. H. Argyris, "Flexure-Torsion Failure of Panels," Aircraft Engineering, June 1954, pp.174-184, and July 1954, pp.213-219.

J. H. Argyris, "Energy Theorems and Structural Analysis, Part I. General Theory," Aircraft Engineering, October 1954, pp.347-356, and November 1954, pp.383-387, 394, and February 1955, pp.42-58, March 1955, pp.80-94.

F. P. Cozzone, "Bending Strength in the Plastic Range," Journal of Aeronautical Sciences, May 1943, pp.137-151.

H. B. Crockett, "Predicting Stiffener and Stiffened Panel Crippling Stresses," Journal of Aeronautical Sciences, November 1942, pp.501-509.

J. E. Duberg, "A Numerical Procedure for the Stress Analysis of Stiffened Shells," Journal of the Aeronautical Sciences, Volume 16, Number 8, August 1949, pp.451-462.

J. C. Ekval, "Static Strength Analysis of Pin-Loaded Lugs," Journal of Aircraft, Vol. 23, No. 5, May 1986, pp.438-443.

S. J. Garvey, "The Quadrilateral 'Shear' Panel, The Peculiar Stressing Problems Arising in the Structure of the Non-Rectangular Swept Wing," Aircraft Engineering, May 1951, p.134-135, 144.

G. Gerard," Secant Modulus Method for Determining Plate Instability Above the Proportional Limit," Journal of the Aeronautical Sciences, January 1946, pp.38-48.

G. Gerard, "Effective Width of Elastically Supported Flat Plates," Journal of the Aeronautical Sciences, October 1946, pp.518-524.

G. Gerard, "The Crippling Stremgth of Compression Elements," Journal of Aeronautical Sciences, January 1958, pp.37-52.

A. F. Grisham, "A Method for Including Post-Buckling of Plate Elements in the Internal Loads Analysis of Any Complex Structure Idealized Using Finite Element Analysis Methods," AIAA Paper No.78-515.

L. J. Hart-Smith, "Easily Assembled Structurally Efficient Joints in Metallic Aircraft Structures," Proceedings of the 18th Symposium of the Committee on Aeronautical Fatigue, 3-5 May, 1995, Melbourne, Australia, pp.331-352.

P. Hoogenboom and J. Blaauwendraad, "Quadrilateral Shear Panel," Engineering Structures 22, 2000, p.1690-1698.

H. Huth, "Influence of Fastener Flexibility on the Prediction of Load Transfer and Fatiue Life for Multiple-Row Joints," Fatigue in Mechanically Fastened Composite and Metallic Joints, ASTM STP 927, 1986, pp.221-250.

M. A. Melcon and A. F. Enshrud, "Analysis of Stiffened Curved Panels Under Shear and Compression," Journal of Aeronautical Sciences, February 1953, pp.111-119.

M. A. Melcon and F. M. Hoblit," Developments in the Analysis of Lugs and Shear Pins," Product Engineering, 24, May 1953, pp.160-170.

R. M. Mello, R. E. Sherrer and M. D. Musgrove, "Intermediate Diagonal Tension Field Shear Beam Development for the SST," Journal of Aircraft, Volume 9, No.7, July, 1972, pp.470-476.

R. Needham, "The Ultimate Strength of Aluminum-Alloy Formed Structural Shapes in Compression," Journal of Aeronautical Sciences, April 1954, pp.217-229.

F. R. Shanley, "Inelastic Column Theory," Journal of the Aeronautical Sciences, May 1947, pp.261-268.

T. Swift, "Damage Tolerance in Pressurized Fuselages," 11th Plantema Memorial Lecture, Proceedings of the 14th Symposium of the International Committee on Aeronautical Fatigue, 8-12 June, 1987, Ottawa, Canada,

M. J. Turner, R. W. Clough, H. C. Martin and L. J. Topp, "Stiffness and Deflection Analysis of Complex Structures," Journal of the Aeronautical Sciences, Semtember 1956, pp.805-823, 854.

Ian Taig, "Rules for Modelling Structures"

R. W. Westrup, "Some Effects of Curvature on Frames," Journal of the Aeronautical Sciences, Semtember 1958, pp.567-572.

S. Yusuff, "Buckling Phenomena of Stiffened Panels," Journal of the Aero/space Sciences, August 1958, pp.507-514.

"Stress Course for Liasion Engineers," USAF Reserve Officers ABDR Training Program.

"Solutions to Problems," USAF Reserve Officers ABDR Training Program.

滝敏美，「表計算ソフトの最適化機能を用いた構造問題へのエネルギ法の直接解法の適用」，第50回構造強度に関する講演会講演集，2008年．