MIL-HDBK-5H 1 December 1998

Transcription

1 . 1.2 ' = Column material compressive yield stress Compressive yield stress (std) ' 1.1 K = Correction Factor F ' c Maximum test column Stress = F ' cy Column material compressive yield stress % '#" " -./0 A bibliography of information on thin-walled and stiffened thin-walled sections is contained in References 1.7.1(a) and (b) ASTM E9-89a, Standard Test Methods for Compression Testing at Metallic Materials at Room Temperature Goodman, S., and Russell, S. 13., U.S. Air Force, Poisson, Ratio of Aircraft Sheet Materials for Large Strain, WADCTR 53-7, 58 pp (June 1953) Hyler, W. S., An Evaluation of Compression-Testing Techniques for Determining Elevated-Temperature Properties of Titanium Sheet, Titanium Metallurgical Laboratory Report No. 43, Battelle Memorial Institute, 38 pp, Appendix 28 pp (June 8, 1956) Stange, A. H., Ramberg, W., and Back, G., Torsion Tests of Tubes, National Advisory Committee for Aeronautics, Report No. 601, pp (February 1937) Stickley, G. W., and Moore, A. A., Effects of Lubrication and Pin Surface on Bearing Strengths of Aluminum and Magnesium Alloys, Materials Research and Standards, 2, (9), pp (September 1962). 1-39

2 (a) (b) (a) (b) Rice, Richard, Reference Document for the Analysis of Creep and Stress Rupture Data in MIL-HDBK-5", AFWAL-TR (September 1991). Aarnes, M. N., and Tuttle, M. M., Presentation of Creep Data for Design Purposes, ASD Technical Report (June 1961) (MCIC 45114). Grover, H. J., Fatigue of Aircraft Structures, Prepared for Naval Air Systems Command, Department of the Navy, 335 pp (1966). Osgood, C. C., Fatigue Design, Wiley-Interscience, a Division of John Wiley and Sons, Inc., 523 pp (1970) Bert, C. W., Mills, E. J., and Hyler, W. S., Mechanical Properties of Aerospace Structural Alloys Under Biaxial-Stress Conditions, AFML-TR (August 1966) (a) (b) (c) Brown, W. F., Jr., and Srawley, J. E., Plane-Strain Crack Toughness Testing of High Strength Metallic Materials, ASTM Special Technical Publication No. 410, American Society for Testing and Materials, Philadelphia (1967). Fracture Toughness Testing and Its Applications, ASTM Special Technical Publication No. 381, American Society for Testing and Materials, Philadelphia (1965). Standard Method of Test for Plane-Strain Fracture Toughness of Metallic Materials, ASTM E Cozzone, F. P., Bending Strength in the Plastic Range, Journal of the Aeronautical Sciences, 10, pp (1943) (a) (b) (c) Dieter, G. E., Jr., Mechanical Metallurgy, McGraw-Hill Book Company, Inc., 615 pp (1961). Freudenthal, A. M., The Inelastic Behavior of Engineering Materials and Structures, John Wiley and Sons, Inc., New York, 587 pp (1950). Parker, E. R., Brittle Behavior of Engineering Structures, John Wiley and Sons, Inc., New York, 323 pp (1957) Lundquist, E. E., Strength Tests of Thin-Walled Duralumin Cylinders in Pure Bending, U.S. National Advisory Committee for Aeronautics, Technical Note No. 479, 17 pp (December 1933) (a) (b) Hill, H. N., and Clark, J. W., Straight-Line Column Formulas for Aluminum Alloys, Aluminum Company of America, Aluminum Research Laboratories, Technical Paper No. 12, 8 pp (1955). AFFDL-TR-69-42, Stress Analysis Manual, Air Force Flight Dynamics Laboratory, Air Force Systems Command, Wright-Patterson Air Force Base (February 1970) (c) Astronautic Structure Manual, George C. Marshall Space Flight Center (August 15, 1970) (d) Niles, A. S., and Newell, J. S., Airplane Structure, 2, Third Edition, John Wiley and Sons (1943). 1-40

3 1.7.1(a) 1.7.1(b) Index of Aircraft Structures Research Reports, U.S. National Advisory Committee for Aeronautics, Index No. 7E29, 40 pp (June 1947). Gerard, and Becker, H., Handbook of Structural Stability, National Advisory Committee for Aeronautics Technical Note, Nos. 3781, 102 pp (July 1957); 3782, 72 pp (July 1957); 3783, 154 pp (August 1957); 3784, 93 pp (August 1957), and 3785, 89 pp (August 1957). 1-41

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