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Metals -- Fatigue

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Fatigue of metals
Metal fatigue

Filed under: Metals -- Fatigue

A Theory for the Effect of Mean Stress on Fatigue of Metals Under Combined Torsion and Axial Load or Bending (1958), by William N. Findley (page images at HathiTrust)
Fatigue and Stress Rupture Properties of Inconel 713C, V-57C and Titanium Alloys 7A1-3Mo-Ti and MST 821 (8A1-2Cb-1Ta-Ti) (Wright-Patterson Air Force Base, Ohio: Wright Air Development Division, Air Research and Development Command, U. S. Air Force, 1960), by A. E. Cers and A. A. Blatherwick (page images at HathiTrust)
Manual on fatigue testing. ([publisher not identified], 1950), by American Society for Testing Materials. Committee E-9 on Fatigue (page images at HathiTrust)
Fatigue of metals and structures ([U. S. Govt. Print. Off.], 1957), by Battelle Memorial Institute and Horace John Grover (page images at HathiTrust)
Prevention of fracture in ship structure : March 30-31, 1995, Washington, D.C. (Ship Structure Committee ;, 1997), by Assembly of Engineering (U.S.). Marine Board and United States. Ship Structure Committee (page images at HathiTrust)
Relevance of fatigue tests to cold leg piping (Nuclear Regulatory Commission, Office of Nuclear Regulatory Research, Division of Reactor Safety Research, 1978), by M. E. Mayfield, R. J. Eiber, E. C. Rodabaugh, and U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research (page images at HathiTrust)
Temperature based stress analysis of notched members (University of Wisconsin, 1978), by Eric Hopkins Jordan (page images at HathiTrust; US access only)
Fatigue properties of manganese-copper damping alloys (U.S. Dept. of the Interior, Bureau of Mines, 1961), by J. W. Jensen, D. F. Walsh, and A. E. Schwaneke (page images at HathiTrust)
Fatigue of metals and structures (Bureau of Naval Weapons, Department of the Navy, 1960), by H. J. Grover, L. R. Jackson, S. A. Gordon, United States Bureau of Naval Weapons, and Battelle Memorial Institute (page images at HathiTrust)
Fatigue of metals and structures (U. S. Govt. Print. Off., 1954), by Battelle Memorial Institute and H. J. Grover (page images at HathiTrust)
Mechanical failures of metals in service (U.S. Govt. Print. Off.], 1954), by John A. Bennett and G. Willard Quick (page images at HathiTrust)
A theory of the non-linear influence of normal stress on fatigue under combined stresses (Engineering Materials Research Laboratory, Division of Engineering, Brown University, 1956), by J. J. Coleman and William Nichols Findley (page images at HathiTrust)
Energy versus stress theories for combined stress; a fatigue experiment using a rotating disc (Engineering Materials Research Laboratory, Division of Engineering, Brown University, 1958), by William N. Findley (page images at HathiTrust)
Modern installation for testing of large assemblies under static and fatigue loading. Description of installation at Fritz Engineering laboratory, Lehigh University, Bethlehem, Pennsylvania (Fritz Engineering Laboratory, Dept. of Civil Engineering, Lehigh University, 1956), by Bruno Thürlimann and W. J. Eney (page images at HathiTrust)
Fatigue tests of plate joints and bolted lugs. ARO project. Final report, September 30, 1954. (Cornell University [Dept. of Engineering Mechanics and Materials, 1954), by J. O. Jeffrey and Cornell University. School of Mechanical Engineering (page images at HathiTrust)
Modified theories of fatigue failure under combined stress (Urbana, 1954), by William N. Findley and P. N. Mathur (page images at HathiTrust)
Interim summary report on the development program for resistance, spot and seam welding of aluminum alloys. Phase III: Development and standardization of design criteria. (Akron, Ohio, 1956), by Goodyear Aircraft Corporation (page images at HathiTrust; US access only)
Fatigue, creep, and rupture properties of the alloys Udimet 500, Hastelloy R-235, and GMR-235. (Wright Air development Center, Air Research and Development Command, U.S. Air Force, 1958), by F.H. Vitovec (page images at HathiTrust)
Investigation of the fatigue properties of molybdenum under various conditions of temperature, coatings, and stress concentration (Wright-Patterson Air Force Base, Ohio, Wright Air Development Division, Air Research and Development Command, U.S. Air Force, 1960 [i.e. 1961], 1961), by Battelle Memorial Institute, George D. Haley, H. J. Grover, Robert Isaac Jaffee, Dean N. Williams, Alexander Arthur Mittenbergs, United States. Air Force. Air Research and Development Command, and United States. Wright Air Development Division (page images at HathiTrust)
Fatigue properties of magnesium alloy forgings. (Wright Air Development Division, Air Research and Development Command, U. S. Air Force, 1960), by Evan Henry Schuette (page images at HathiTrust)
Fatigue behavior of 2014-T6, 7075-T6 and 7079-T6 aluminum alloy regular hand forgings (Wright Air Development Center, Air Research and Development Command, U.S. Air Force, 1960), by D. A. Paul and Douglas Y. Wang (page images at HathiTrust)
Design of specimens for short-time "fatigue" tests (U.S. Dept. of Commerce, Bureau of Standards :, 1924), by Louis Bryant Tuckerman, Clyde Stanley Aitchison, and United States. National Bureau of Standards (page images at HathiTrust)
Cyclic fatigue damage characteristics observed for simple loadings extended to multiaxial life prediction (Lewis Research Center ;, 1988), by David J. Jones, Peter Kurath, University of Illinois at Urbana-Champaign, and Lewis Research Center (page images at HathiTrust)
An extension of plane strain analysis (National Aeronautics and Space Administration ;, 1966), by Kwan Rim, Roger O. Stafford, University of Iowa, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Life prediction of thermomechanical fatigue using total strain version of strainrange partitioning (SRP) : a proposal (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by James F. Saltsman, Gary R. Halford, and Lewis Research Center (page images at HathiTrust)
Rolling-element fatigue life of AISI M-50 and 18-4-1 balls (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Richard J. Parker, Erwin V. Zaretsky, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Effect of carbide distribution on rolling-element fatigue life of AMS 5749 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Richard J. Parker, Eric N. Bamberger, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Effect of shot peening on surface fatigue life of carburized and hardened AISI 9310 spur gears (National Aeronautics and Space Administration, Scientific and Technical Branch ;, 1982), by Dennis P. Townsend, Erwin V. Zaretsky, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Friction, wear, and auger analysis of iron implanted with 1.5-MeV nitrogen ions (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by John Ferrante, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
Some considerations in the fatigue design of launch and spacecraft structures (National Aeronautics and Space Administration ;, 1965), by R. H. Christensen, R. J. Bellinfante, and Douglas Aircraft Company (page images at HathiTrust)
Metal fatigue (NASA, 1965), by F. B. Stulen, W. C. Schulte, J. H. Redfern, Curtiss-Wright Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Model for flaw-induced fracture in non-ductile materials (National Aeronautics and Space Administration, 1966), by H. U. Schuerch, Astro Research Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Mechanism of the atmospheric interaction with the fatigue of metals (National Aeronautics and Space Administration, 1968), by M. J. Hordon and M. A. Wright (page images at HathiTrust; US access only)
Fatigue evaluation of composite-reinforced, integrally stiffened metal panels : summary (National Aeronautics and Space Administration ;, 1973), by C. E. Dumesnil, Langley Research Center, and Vought Aeronautics Company (page images at HathiTrust)
Analysis of fatigue crack propagation (National Aeronautics and Space Administration ;, 1972), by H. W. Liu (page images at HathiTrust)
High temperature low cycle fatigue mechanisms for a nickel-base and a copper-base alloy (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), by Chin-I. Shih, University of Cincinnati. Dept. of Materials Science and Metallurgical Engineering, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Lewis Research Center (page images at HathiTrust)
Residual strength of five boron/aluminum laminates with crack-like notches after fatigue loading (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by R. A. Simonds, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Virginia Polytechnic Institute and State University, and Langley Research Center (page images at HathiTrust)
Environmental crack-growth behavior of high-strength pressure vessel alloys (National Aeronautics and Space Administration ;, 1975), by Royce G. Forman, Lyndon B. Johnson Space Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-2331 (National Aeronautics and Space Administration :, 1964), by C. M. Hudson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Use of strainrange partitioning to predict high-temperature low-cycle fatigue life (National Aeronautics and Space Administration ;, 1976), by Marvin H. Hirschberg, Gary R. Halford, and Lewis Research Center (page images at HathiTrust)
Predicted characteristics of an optimized series-hybrid conical hydrostatic ball bearing (National Aeronautics and Space Administration, 1971), by Lester J. Nypan, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
NASA TN D-6691 (National Aeronautics and Space Administration :, 1972), by Howard G. Nelson, Ames Research Center, Los Angeles University of California, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Application of a double linear damage rule to cumulative fatigue (National Aeronautics and Space Administration, 1967), by S. S. Manson, C. Robert Ensign, John C. Freche, and Lewis Research Center (page images at HathiTrust)
Effect of carbide size, area, and density on rolling-element fatigue (National Aeronautics and Space Administration ;, 1972), by James L. Chevalier, Erwin V. Zaretsky, U.S. Army Air Mobility Research and Development Laboratory, and Lewis Research Center (page images at HathiTrust)
Elevated-temperature combined stress-rupture plus fatigue strength of waspaloy having having different aging treatments and/or molybedenum contents (National Advisory Committee for Aeronautics, 1958), by Charles A. Hoffman, M. B. Hornak, United States National Advisory Committee for Aeronautics, and Lewis Research Center (page images at HathiTrust)
The failure of metals under internal and prolonged stress, a general discussion. (Faraday Society, 1921), by F. S. Spiers (page images at HathiTrust; US access only)
Sonic fatigue design techniques for advanced composite aircraft structures : final report (Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1980), by I. Holehouse and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Mass spectrometer studies of compound cracking patterns (Technical Information Service, 1951), by Russell Baldock, John R. Sites, Oak Ridge Y-12 Plant, U.S. Atomic Energy Commission, and Oak Ridge National Laboratory (page images at HathiTrust)
Calculation of mechanical behavior of materials through true stress-true strain relationships (Atomics International, 1962), by W. J. Anderson, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
Effect of material damping and stress distribution on the resonant fatigue strength of parts (Wright Air Development Center, Air Research and Development Command, U.S. Air Force, 1955), by Egons R. Podnieks, Benjamin Joseph Lazan, and United States. Wright Air Development Division (page images at HathiTrust)
New methods of measurement of residual stress. (Wright Air Development Center, Air Research and Development Command, U. S. Air Force, 1954), by R. F. Brodrick (page images at HathiTrust)
Low cycle fatigue evaluation of primary piping materials in a BWR environment (San Jose, California : Boiling Water Reactor Systems Department, General Electric Company, 1977., 1977), by D. A. Hale, General Electric Company. Boiling Water Reactor Systems Department, and U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Metallurgy and Materials Research Branch (page images at HathiTrust)
Local stress-strain approach to cumulative fatigue damage analysis : final report (Dept. of Theoretical and Applied Mechanics, University of Illinois, 1974), by JoDean Morrow, N. E. Dowling, J. F. Martin, and University of Illinois at Urbana-Champaign. Department of Theoretical and Applied Mechanics (page images at HathiTrust; US access only)
Fatigue failure under combinations of stresses (Dept. of Theoretical and Applied Mechanics, University of Illinois, 1954), by William N. Findley, D. E. Martin, Prem Narain Mathur, and University of Illinois at Urbana-Champaign. Dept. of Theoretical and Applied Mechanics (page images at HathiTrust; US access only)
Metal fatigue and its recognition (Civil Aeronautics Board, Bureau of Safety, 1963), by Frank R. Stone and United States. Civil Aeronautics Board. Bureau of Safety (page images at HathiTrust)
Stress-corrosion cracking : a nontechnical introduction to the problem (Columbus, Ohio : Defense Metals Information Center, Battelle Memorial Institute, 1961., 1961), by Warren E. Berry and Defense Metals Information Center (U.S.) (page images at HathiTrust)
A survey report on fatigue in cannon bores (Columbus, Ohio : Defense Metals Information Center, Battelle Memorial Institute, 1967., 1967), by H. J. Grover and Defense Metals Information Center (U.S.) (page images at HathiTrust)
Estimate of probability of crack detection from service difficulty report data (FAA Technical Center ;, 1994), by John C. Brewer, John A. Volpe National Transportation Systems Center (U.S.), and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
Enquête sur la fatigue des métaux (Paris : H. Dunod et E. Pinat, 1910., 1910), by A. Fejtö (page images at HathiTrust; US access only)
An investigation of the fatigue characteristics of leaded alloy steels (Dept. of Theoretical and Applied Mechanics, Univ. of Illinois, 1956), by George William Brock and George Morton Sinclair (page images at HathiTrust; US access only)
Investigation of shell cracking on the steam generators at Indian Point, unit no. 3 (Washington, D. C. : U.S. Nuclear Regulatory Commission, 1983., 1983), by C. Czajkowski, Brookhaven National Laboratory. Department of Nuclear Energy, and U.S. Nuclear Regulatory Commission. Office of Nuclear Reactor Regulation. Division of Engineering (page images at HathiTrust)
Crack growth evaluation for small cracks in reactor coolant piping (Washington, D. C. : U.S. Nuclear Regulatory Commission, 1983., 1983), by F. A. Simonen, D. Jones, T. P. Forte, M. E. Mayfield, Pacific Northwest Laboratory, and U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering Technology (page images at HathiTrust)
Fatigue crack growth rates of A 508-2 steel in pressurized, high temperature water (The Commission, 1983), by W. H. Cullen, Inc ENSA, Materials Engineering Associates, and U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering Technology (page images at HathiTrust)
Constant extension rate testing of SA302 Grade B Material in Neutral and chloride solutions (Washington, D.C. : Division of Engineering, Office of Nuclear Reactor Regulation, U.S. Nuclear Regulatory Commission, 1984., 1984), by C. Czajkowski, Brookhaven National Laboratory, and U.S. Nuclear Regulatory Commission. Office of Nuclear Reactor Regulation. Division of Engineering (page images at HathiTrust)
Reduction of the endurance limit as a result of stress interaction in fatugue (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, U.S. Air Force, 1961., 1961), by Robert A. Heller, United States. Air Force. Air Research and Development Command, Columbia University, and Wright Air Development Division (page images at HathiTrust)
Aspects of the response of structures subject to sonic fatigue (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, U.S. Air Force, 1961., 1961), by Hassel C. Schjelderup, Arnold E. Galef, United States. Air Force. Air Research and Development Command, Wright Air Development Division, and National Engineering Science Company (page images at HathiTrust)
A study of the influence of geometry on the strength of fatigue cracked panels (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), by E. K. Walker, Northrop Corporation, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Large amplitude response of complex structures due to high intensity noise (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), by C. Mei, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
The statistical nature of fatigue crack propagation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978., 1978), by D. A. Virkler, P. K. Goel, B. M. Hillberry, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Purdue University. School of Mechanical Engineering (page images at HathiTrust)
Durability methods development. Volume 3, Structural durability survey: state-of-the-art assessment (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), by B. J. Pendley, S. D. Manning, S. P. Henslee, Air Force Flight Dynamics Laboratory (U.S.), and General Dynamics Corporation (page images at HathiTrust)
The relationship of earliest failures to fleet size and "parent" population (Wright-Patterson Air Force, Ohio : Air Force Materials Laboratory, Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), by Robert A. Heller, A. S. Heller, Air Force Materials Laboratory (U.S.), United States. Air Force. Systems Command, and Columbia University. Department of Civil Engineering and Engineering Mechanics (page images at HathiTrust)
The cyclic state of materials and the relationship to mechanical properties and fatigue (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, XXXX1966., 1966), by Dewey G. Younger and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Durability methods development. Volume 4, Initial quality representation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), by Masanobu Shinozuka, Air Force Flight Dynamics Laboratory (U.S.), and Modern Analysis Inc (page images at HathiTrust)
The early detection of fatigue damage (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by John F. Moore, George Martin, Schillings Tsang, Air Force Materials Laboratory (U.S.), and North American Rockwell Corporation (page images at HathiTrust)
Further investigation of notch sensitivity of refractory metals. (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1965., 1962), by Battelle Memorial Institute and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
Durability methods development. Volume 5, Durability analysis methodology development (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), by J. N. Yang, W. R. Garver, S. D. Manning, Air Force Flight Dynamics Laboratory (U.S.), General Dynamics Corporation, and George Washington University (page images at HathiTrust)
Sonic fatigue design techniques for advanced composite aircraft structures : Final report (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), by Ian Holehouse, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Inc Rohr Industries (page images at HathiTrust)
The effect of stress concentration on the fracture and deformation characteristics of ceramics and metals (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by Volker Weiss, United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States, and Syracuse University (page images at HathiTrust)
Research on techniques of establishing random type fatigue curves for broad band sonic loading (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by J. R. Fuller, United States. Air Force. Systems Command. Aeronautical Systems Division, Boeing Company. Transport Division, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Response of nonlinear structural panels subjected to high intensity noise (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), by C. Mei, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and University of Missouri--Rolla. Mechanical Engineering Department (page images at HathiTrust)
Test methods for mechanical properties of anisotropic materials (Beryllium sheet) (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), by Raymond W. Fenn, B. M. Lempriere, W. C. Kinder, D. D. Crooks, Air Force Materials Laboratory (U.S.), and Lockheed Missiles and Space Company (page images at HathiTrust)
Effects of variations in coldworking repair procedures on flaw growth and structural life (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), by J. M. Pearson-Smith, J. M. Potter, Air Force Flight Dynamics Laboratory (U.S.), and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
Investigation of the distribution of tension in notched construction elements (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by H. Neuber, United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States, and Technische Hochschule München (page images at HathiTrust)
The effect of cadmium plating on aircraft steels under stress concentration at elevated temperatures (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), by E. M. Kennedy and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
Structural evaluation of superplastic sluminum. Part 1. Mechanical, corrosion, metallurgical data (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), by Hadassah C. Lipsius, Alvin Shames, Julius Stock, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Development of a mathematical model for predicting the percentage fatigue life increase resulting from shot peened components. Phase I (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), by Roger S. Simpson, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Effects of underloads on fatigue crack growth. Volume II, Data tabulations (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), by W. M. McGee, T. M. Hsu, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command, and Lockheed-Georgia Company (page images at HathiTrust)

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