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Thermal stresses

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Filed under: Thermal stresses

Thermal stresses, with applications to airplanes, missiles, turbines and nuclear reactors. (McGraw-Hill, 1957), by Buford Echols Gatewood (page images at HathiTrust)
Investigation and evaluation of cracking incidents in piping in pressurized water reactors (U.S. Nuclear Regulatory Commission :, 1980), by U.S. Nuclear Regulatory Commission and PWR Pipe Crack Study Group (U.S.) (page images at HathiTrust)
Multiloop Integral System Test (MIST) : final report (Division of Systems Research, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission :, 1989), by G. O. Geissler, J. R. Gloudemans, Babcock & Wilcox Owners Group, Electric Power Research Institute, U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Systems Research, Babcock & Wilcox Company. Alliance Research Center, and Babcock & Wilcox Company. Nuclear Power Division (page images at HathiTrust)
Properties of reactor materials at constant true strain rates : progress report, July 1, 1977 - June 30, 1978 (U.S. Nuclear Regulatory Commission, Office of Nuclear Regulatory Research, Division of Reactor Safety Research ;, 1978), by C. S. Hartley, University of Florida. Department of Materials Science and Engineering, and U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research (page images at HathiTrust)
Supplemental data on coefficient of thermal expansion, modulus of elasticity and Poisson's ratio as functions of temperature (Argonne National Laboratory, 1960), by J. C. Heap, U.S. Atomic Energy Commission, and Argonne National Laboratory. Reactor Engineering Division (page images at HathiTrust)
Analysis of stresses in a rock disk subjected to peripheral thermal shock (U.S. Dept. of the Interior, Bureau of Mines, 1966), by T. S. Chen, Robert Lawrence Marovelli, and United States Bureau of Mines (page images at HathiTrust)
Some properties of beryllium oxide (Lawrence Radiation Laboratory, 1961), by J. Lillie and Lawrence Radiation Laboratory (page images at HathiTrust)
Two-year Wisconsin thermal loads for roof assemblies and wood, wood-plastic composite, and fiberglass shingles (U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 2005), by Jerrold E. Winandy, Cherilyn A. Hatfield, Michael Grambsch, and Forest Products Laboratory (U.S.) (page images at HathiTrust)
The dependence of thermal stresses in cylindrical reactor fuel elements upon the method of cooling (U.S. Atomic Energy Commission, 1957), by K. R. Merckx, U.S. Atomic Energy Commission, United States. Energy Research and Development Administration, Hanford Works, and Hanford Atomic Products Operation. Reactor and Fuels Research and Development Operation (page images at HathiTrust)
Thermal stresses in beryllium (Oak Ridge National Laboratory, 1950), by H. C. Savage, U.S. Atomic Energy Commission, and Oak Ridge National Laboratory Technical Division Engineering Development Section (page images at HathiTrust)
Factors affecting thermal shock resistance of polyphase ceramic bodies (Wright Air Development Division, Air Research and Development Command, U. S. Air Force, 1961), by Carborundum Company, A. Z. Chaberski, D. P. H. Hasselman, and P. T. B. Shaffer (page images at HathiTrust)
Thermal buckling of circular cylindrical and conical thin-walled shells (Wright Air Development Center, Air Research and Development Command, U.S. Air Force, 1958), by David Abir (page images at HathiTrust)
Combined effects of axial load, thermal stress, and creep in flat plates (Wright Air Development Center, Air Research and Development Command, U. S. Air Force, 1958), by P. C. Huang and C. J. Van Der Maas (page images at HathiTrust)
On thermal stresses, strains, and warping (U.S. Atomic Energy Commission. Technical Information Division, 1944), by F. H. Murray, G. Young, Clinton Laboratories, and U.S. Atomic Energy Commission (page images at HathiTrust)
Thermal stresses and strains in a finite cylinder with no surface forces (U.S. Atomic Energy Commission. Technical Information Division, 1945), by F. H. Murray, Clinton Laboratories, and U.S. Atomic Energy Commission (page images at HathiTrust)
Temperature gradient and thermal stresses in bodies with uniformly distributed volume heat sources. (Technical Information Service, 1955), by F. A. Field (page images at HathiTrust)
Effects of variables upon pyrotechnically induced shock response spectra : part II (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by James Lee Smith and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
Preliminary study of thermomechanical fatigue of polycrystalline MAR-M 200 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Robert C. Bill and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Effects of thermal cycling on graphite-fiber-reinforced 6061 aluminum (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Gregory A. Dries, Stephen S. Tompkins, and Langley Research Center (page images at HathiTrust)
Elastic-plastic finite-element analysis of thermally cycled double-edge wedge specimens (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Albert Kaufman, Larry E. Hunt, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Gas turbine ceramic-coated-vane concept with convection-cooled porus metal core (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Albert F. Kascak, Lewis Research Center, Propulsion Laboratory (U.S.), and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Materials constitutive modes for nonlinear analysis of thermally cycled structures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Albert Kaufman, Larry E. Hunt, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Elastic-plastic finite-element analysis of thermally cycled single-edge wedge specimens (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Albert Kaufman, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
MEGA16 - computer program for analysis and extrapolation of stress-rupture data (National Aeronautics and Space Administration, Scientific and Technical Branch ;, 1981), by C. Robert Ensign, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Flightweight radiantly and actively cooled panel : thermal and structural performance (National Aeronautics and Space Administation, Scientific and Technical Information Branch ;, 1982), by Charles P. Shore, H. Neale Kelly, Robert J. Nowak, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Effect of strain isolator pad modulus on inplane strain in shuttle orbiter thermal protection system tiles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by James Wayne Sawyer and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Supersonic flutter of a thermally stressed flat plate with edge stiffeners (National Aeronautics and Space Administration ;, 1970), by Harmohan Singh Singh, Charles Libove, Electronics Research Center (U.S.), and Syracuse University (page images at HathiTrust)
Free vibrations of thermally stressed orthotropic plates with various boundary conditions (National Aeronautics and Space Administration ;, 1973), by C. D. Bailey, James C. Greetham, Langley Research Center, and Ohio State University. Research Foundation (page images at HathiTrust)
Design data for brazed Rene ́41 honeycomb sandwich (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Andrew K. Hepler, Boeing Aerospace Company, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Cryogenic performance of slotted brazed Rene ́41 honeycomb panels (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), by Andrew K. Hepler, Allan R. Swegle, Langley Research Center, Boeing Aerospace Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Improved finite element methodology for integrated thermal structural analysis (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Pramote Dechaumphai, Earl A. Thornton, Old Dominion University. Research Foundation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Design and fabrication of a stringer stiffened discrete tube actively cooled panel for a hypersonic aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Frank M. Anthony, Robert G. Helenbrook, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Nonlinear effects on composite laminate thermal expansion (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Z. Hashin, R. Byron Pipes, B. W. Rosen, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
An improved method for optimum design of mechanically and thermally loaded structures (National Aeronautics and Space Administration ;, 1975), by Howard M. Adelman, R. Narayanaswami, Joanne L. Walsh, and Langley Research Center (page images at HathiTrust)
Thermal fatigue of ductile materials. III, Behavior of crucible 422 steel (National Aeronautics and Space Administration, 1959), by Francis J. Clauss and Lewis Research Center (page images at HathiTrust)
NASA TN D-5867 (National Aeronautics and Space Administration :, 1970), by Han-Shou Liu, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TN D-5926 (National Aeronautics and Space Administration :, 1970), by Charles A. Hoffman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Thermal-stress fatigue cracking of turbine buckets operated at 1700° F in a turbojet engine with long periods of operation between starts (National Aeronautics and Space Administration, 1960), by Robert A. Signorelli, William J. Waters, James R. Johnston, and Lewis Research Center (page images at HathiTrust)
NASA TN D-6251 (National Aeronautics and Space Administration ;, 1971), by William R. Jones, William F. Hady, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Minimum-weight analysis of symmetrical-multiweb-beam structures subjected to thermal stress (National Aeronautics and Space Administration, 1959), by Robert R. McWithey and Langley Research Center (page images at HathiTrust)
A study of methods for simulating the atmosphere entry of vehicles with small-scale models (National Aeronautics and Space Administration, 1960), by Byron L. Swenson and Ames Research Center (page images at HathiTrust)
Range of interface thermal conductance for aircraft joints (National Aeronautics and Space Administration, 1960), by Martin E. Barzelay and Syracuse University (page images at HathiTrust)
NASA TN D-1740 (National Aeronautics and Space Administration, 1963), by Ernest Roberts, Alexander Mendelson, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Establishing allowable temperature gradients for tungsten-uranium dioxide fuel elements using experimental cyclic strain data (National Aeronautics and Space Administration ;, 1968), by Ivan B. Fiero and Lewis Research Center (page images at HathiTrust)
Stresses in perforated sheets due to nonuniform heating (General Electric Company, 1951), by G. Horvay, General Electric Company Knolls Atomic Power Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
Thermal stress in HRT pressure vessel (United States Atomic Energy Commission, Technical Information Extension ;, 1955), by R. E. Aven, Oak Ridge National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
The thermal fracture of ceramic cylinders (Battelle Memorial Institute, 1956), by Winston H. Duckworth, Eugene M. Simons, Eugene Michael Baroody, Allison K. Smalley, U.S. Atomic Energy Commission, and Battelle Memorial Institute (page images at HathiTrust)
Experimental and theoretical determination of thermal stresses in a flat plate (National Advisory Committee for Aeronautics, 1952), by Richard R. Heldenfels, William M. Roberts, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
A table of the cubical expansion of solids (s.n., 1888), by J. G. MacGregor and Royal Society of Canada (page images at HathiTrust)
Relaxation of torsional stresses in stainless steel during irradiation (E.I. du Pont de Nemours & Co., Explosives Dept., Atomic Energy Division, Technical Division, Savannah River Laboratory, 1962), by Richard E. Schreiber, U.S. Atomic Energy Commission, and Savannah River Laboratory (page images at HathiTrust)
Friction and wear of refractory compounds : progress report (General Electric, Aircraft Nuclear Propulsion Dept., Atomic Products Division, 1958), by K. P. Zeman, L. F. Coffin, and General Electric Company. Aircraft Nuclear Propulsion Department. Atomic Products Division (page images at HathiTrust)
Steady-state and transient thermal stresses in a tube subjected to internal heating (General Electric, Aircraft Nuclear Propulsion Dept., Atomic Products Division, 1959), by H.A. Eagle, A.L. Ross, and General Electric Company. Aircraft Nuclear Propulsion Department. Atomic Products Division (page images at HathiTrust)
Steady-state and transient thermal stresses in a tube subjected to internal heating (General Electric, Aircraft Nuclear Propulsion Dept., Atomic Products Division, 1959), by H.A. Eagle, A.L. Ross, and General Electric Company. Aircraft Nuclear Propulsion Department. Atomic Products Division (page images at HathiTrust)
Thermal stresses in tube with axial temperature gradient (General Electric, Aircraft Nuclear Propulsion Dept., Atomic Products Division, 1959), by R. J. Dunholter and General Electric Company. Aircraft Nuclear Propulsion Department. Atomic Products Division (page images at HathiTrust)
Thermal stress analysis of finite sections (General Electric, Aircraft Nuclear Propulsion Dept., Atomic Products Division, 1959), by Arthur L. Ross and General Electric Company. Aircraft Nuclear Propulsion Department. Atomic Products Division (page images at HathiTrust)
Photothermoelasticity techniques and application (General Electric, Nuclear Materials and Propulsion Operation, 1961), by Warren E. Greenwald, U.S. Atomic Energy Commission, and General Electric Company (page images at HathiTrust)
Thermal stresses in hollow cylinders (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Division of Technical Information ; 1954., 1954), by R.A. Powell, H. Poritsky, U.S. Atomic Energy Commission, and General Electric Company (page images at HathiTrust)
Evaluation of transient temperatures and stresses (Knolls Atomic Power Laboratory, General Electric Company ;, 1957), by R. J. Fritz, U.S. Atomic Energy Commission, General Electric Company, and Knolls Atomic Power Laboratory (page images at HathiTrust)
Thermal-stress ratchet mechanism in pressure vessels (Knolls Atomic Power Laboratory, General Electric Company, 1959), by D.R. Miller, U.S. Atomic Energy Commission, General Electric Company, and Knolls Atomic Power Laboratory (page images at HathiTrust)
Structural analysis of a reflux pool-boiler solar receiver (Sandia National Laboratories ;, 1991), by Edward L. Hoffman, Charles M. Stone, Sandia National Laboratories, and Sandia Laboratories (page images at HathiTrust)
Development and implementation of time-dependent cracking material model for concrete (U.S. Army Engineer Waterways Experiment Station ;, 1991), by Sharon B. Garner, Michael I. Hammons, U.S. Army Engineer Waterways Experiment Station, and United States Army Corps of Engineers (page images at HathiTrust)
Transient temperature and thermal stress equations for a homogeneous flat plate heated by multiple pulsed cyclic heat generation (Livermore Research Laboratory, 1953), by D. F. Casey, Lawrence Livermore Laboratory, California Research and Development Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
Bibliography on thermal stresses and low cycle fatigue (Knolls Atomic Power Laboratory, General Electric Co., 1959), by D. R. Miller, General Electric Company, U.S. Atomic Energy Commission, and Knolls Atomic Power Laboratory (page images at HathiTrust)
A general method for the determination of the thermal stresses in a composite medium (United States Atomic Energy Commission, Technical Information Service , 1952), by Julius J. Brandstatter, U.S. Atomic Energy Commission. Technical Information Center, and North American Aviation. Atomics International Division (page images at HathiTrust)
Experimental study of inelastic strains in hollow cylinder of 6061 aluminum subjected to a band of internal pressure (Canoga Park, California : Atomics International, 1965., 1965), by Vincent W. Anderson, U.S. Atomic Energy Commission. Technical Information Center, and North American Aviation. Atomics International Division (page images at HathiTrust)
The true stress-strain properties of brittle materials to 5000° F : final report. (Oak Ridge, Tennessee : United States Atomic Energy Commission, Technical Information Service, 1961., 1961), by U.S. Atomic Energy Commission. Division of Technical Information and Ala.) Southern Research Institute (Birmingham (page images at HathiTrust)
The true stress-strain properties of brittle materials to very high temperatures : final report to U.S. Atomic Energy Commission (1961-1962). (Oak Ridge, Tennessee : United States Atomic Energy Commission, Technical Information Service Extension, 1962., 1962), by U.S. Atomic Energy Commission. Division of Technical Information and Ala.) Southern Research Institute (Birmingham (page images at HathiTrust)
Transient thermal stresses in circular disks (Schenectady, New York : Knolls Atomic Power Laboratory, 1951., 1951), by G. Horvay, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
Transient thermal stresses (Downey, California : Atomic Energy Research Department, North American Aviation, Inc., 1952., 1952), by M. P. Heisler, E. Martin, U.S. Atomic Energy Commission, and North American Aviation (page images at HathiTrust)
Thermal stresses in composite bridge beams : working plan (Virginia Council of Highway Investigation and Research, 1960), by William Zuk and Virginia Council of Highway Investigation and Research (page images at HathiTrust; US access only)
Unresolved safety issues : pressurized thermal shock : oversight hearing before the Subcommittee on Oversight and Investigations of the Committee on Interior and Insular Affairs, House of Representatives, Ninety-seventh Congress, second session, on unresolved safety issues, pressurized thermal shock; hearing held in Washington, D.C., May 7, 1983. (U.S. G.P.O, 1984), by United States. Congress. House. Committee on Interior and Insular Affairs. Subcommittee on Oversight and Investigations (page images at HathiTrust)
Joint AEC-ASME program on thermal stress fatigue (Knolls Atomic Power Laboratory, General Electric Company, 1955), by L. F. Coffin, U.S. Atomic Energy Commission, General Electric Company, and Knolls Atomic Power Laboratory (page images at HathiTrust)
Evaluation of transient temperatures and stresses (Schenectady, New York : Knolls Atomic Power Laboratory, 1953., 1953), by R. J. Fritz, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
Thermal stress in power-producing elements (Los Angeles, California : North American Aviation, Inc., 1948., 1948), by A. S. Thompson, North American Aviation, and U.S. Atomic Energy Commission (page images at HathiTrust)
Formation of a modern ice-push ridge by thermal expansion of lake ice in southeastern Connecticut (CRREL, 1969), by Fred Pessl (page images at HathiTrust)
Control of dimensions in high-strength heat-treated steel parts (Columbus, Ohio : Defense Metals Information Center, Battelle Memorial Institute, 1961., 1961), by A. R. Elsea, A. M. Hall, T. H. Feron, and Defense Metals Information Center (U.S.) (page images at HathiTrust)
Numerical results for Experimental Gas-Cooled Reactor moderator-element stress problems (Battelle Memorial Institute, 1961), by Lewis E. Hulbert, Robert F. Redmond, U.S. Atomic Energy Commission, and Battelle Memorial Institute (page images at HathiTrust)
Pressure and thermal stresses at a pipe attachment to a sphere (Knolls Atomic Power Laboratory, General Electric Company, 1959), by Lorenzo Deagle, U.S. Atomic Energy Commission, General Electric Company, and Knolls Atomic Power Laboratory (page images at HathiTrust)
On thermal stresses, strains, and warping (U.S. Atomic Energy Commission. Technical Information Division, 1950), by F. H. Murray, G. Young, Clinton Laboratories, and U.S. Atomic Energy Commission (page images at HathiTrust)
Thermal stresses and strains in a finite cylinder with no surface forces (U.S. Atomic Energy Commission. Technical Information Division, 1951), by F. H. Murray, Clinton Laboratories, and U.S. Atomic Energy Commission (page images at HathiTrust)
Behavior of a cantilever plate under rapid-heating conditions (National Advisory Committee for Aeronautics, 1955), by Louis F. Vosteen, Kenneth James Fuller, and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
L.O.C.A. simulation in the national research universal reactor program (U.S. Nuclear Regulatory Commission, 1983), by C. L. Mohr, Charles L. Wilson, G. E. Russcher, R. K. Marshall, G. M. Hesson, Pacific Northwest Laboratory, and U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Accident Evaluation (page images at HathiTrust)
L.O.C.A. simulation in the national research universal reactor program (Washington, D. C. : Division of Accident Evaluation, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1984., 1984), by W. N. Rausch, Pacific Northwest Laboratory, and U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Accident Evaluation (page images at HathiTrust)
Detection of small-sized near-surface under-clad cracks for reactor pressure vessels (Washington, D.C. : U.S. Nuclear Regulatory Commission, 1983., 1983), by T. T. Taylor, G. J. Posakony, S. R. Doctor, S. L. Crawford, Pacific Northwest Laboratory, and U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering Technology (page images at HathiTrust)
On the Steady-state thermoelastic problem for the half-space and the thick plate ([United States Air Force, Office of Scientific Research], 1959), by Ian Naismith Sneddon, F. J. Lockett, United States. Air Force. Office of Scientific Research, and Duke University (page images at HathiTrust)
Operating experience with the sodium reactor experiment and its application to the Hallam nuclear power facility (Oak Ridge, Tennessee : USAEC Division of Technical Information Extension, 1961., 1961), by R. J. Beeley, J. E. Mahlmeister, U.S. Atomic Energy Commission. Technical Information Center, and North American Aviation. Atomics International Division (page images at HathiTrust)
Thermal stresses in perforated plates (Schenectady, New York : General Electric Company, Knolls Atomic Power Laboratory, 1951., 1951), by G. Horvay, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
Pressure vessel fracture studies pertaining to PWR LOCA-ECC thermal shock : experiments TSE-3 and TSE-4 and update of TSE-1 and TSE-2 analysis (Oak Ridge, Tennessee : Oak Ridge National Laboratory, Engineering Technology Division, 1977., 1977), by R. D. Cheverton, S. E. Bolt, Oak Ridge National Laboratory. Engineering Technology Division, Union Carbide Corporation, and U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research (page images at HathiTrust)
Effect of static prestrain on the prot-fatigue properties of unnotched and notched materials at room ane elevated temperatures (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1959), by F. H. Vitovec, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
Influence of residual stresses and thermal gradients on mechanism of buckling of shallow spherical shells (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), by Megumi Sunakawa, R. M. Evan-Iwanowski, Air Force Flight Dynamics Laboratory (U.S.), and Syracuse University. Research Institute (page images at HathiTrust)
A technique for obtaining improved real-time holographic interferometric data using pulse modulated illumination (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Structural Analysis Group, Structures Division, Air Force Systems Command, United States Air Force, 1971., 1971), by Frank D. Adams, Gene E. Maddux, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Investigation of weldability of hot-work tool steels (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), by N. A. Sinclair, R. P. Sopher, J. G. Maciora, United States. Air Force. Systems Command. Aeronautical Systems Division, United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States, and General Dynamics Corporation. Electric Boat Division (page images at HathiTrust)
Proceedings of Symposium on Aerothermoelasticity ; 30-31 October and 1 November 1961 (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, [1962], 1962), by David M. Jones and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
Allowable stresses for elevated temperature structures (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by C. G. Swanson, P. C. Huang, C. J. Van der Maas, United States. Air Force. Systems Command. Aeronautical Systems Division, Martin Marietta Corporation. Baltimore Division, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Development of experimental testing programs to verify thermal stress analysis (Wright-Patterson AIr Force Base, Ohio : Air Force Flight Dynamicas Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), by B. E. Gatewood, B. H. Ulrich, A. R. Glaser, Ohio State University. Department of Aeronautical and Astronautical Engineering, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Elasto-plastic analysis of structures under load and two-dimensional temperature distributions. Volume 3, Experimental evaluation of the general time-dependent analysis (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by R. J. Edwards, United States. Air Force. Systems Command. Aeronautical Systems Division, Air Force Flight Dynamics Laboratory (U.S.), and Martin Marietta Corporation. Baltimore Division (page images at HathiTrust)
Measuring accuracy in creep tests : Part II. Influence of thermal stresses (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), by Arne Mellgren, Wright Air Development Center, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
Materials central-ASM metallurgical educational lectures (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by Mars G. Fontana, W. Payne, B. D. McConnell, Tong Liu, A. M. Hall, United States. Air Force. Systems Command. Aeronautical Systems Division, and United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States (page images at HathiTrust)
A sensitive weighing device (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1955., 1955), by Alfred T. Kornfield, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and St. Louis University. School of Medicine (page images at HathiTrust)
Thermo-structural analysis manual. Volume I (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, U.S. Air Force, 1962., 1962), by H. Switzky, M. Noiman, Marvin J. Forray, United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processes, and Republic Aviation Corporation (page images at HathiTrust)
Theory of on-axis intensity distribution in thermal lensing (LQ-10 high power laser window program) (L.G. Hanscom Field, Massachusetts : Air Force Cambridge Research Laboratories, Air Force System Command, United States Air Force, 1972., 1972), by Bernard Bendow, Peter D. Gianino, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Thermo-structural analysis manual. Volume II (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, U.S. Air Force, 1962., 1962), by Marvin J. Forray, M. Noiman, H. Switzky, United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processes, and Republic Aviation Corporation (page images at HathiTrust)
Optical performance evaluation of infrared transmitting materials (LQ-10 high power laser window program) (L.G. Hanscom Field, Massachusetts : Air Force Cambridge Research Laboratories, Air Force System Command, United States Air Force, 1972., 1972), by Bernard Bendow, Peter D. Gianino, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Transient coupled thermoplastic boundary value problems in the half-space. (Defense Technical Information Center, 1961), by Irwin S. Tolins, Bruno A. Boley, and Columbia Univ. New York Inst. of Flight Structures (page images at HathiTrust)
Thermal stresses in coatings on carbon-carbon composites (National Aeronautics and Space Administration, Langley Research Center, 1996), by Andreas W. Obst, M. W. Hyer, and Langley Research Center (page images at HathiTrust)
Effects of severe thermal and stress histories on material strength - rate process theory approach AISI 301 extra hard, PH 15-7 Mo RH, RENE' 41, 7075-T6 (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems DIvision, Air Force Systems Command, United States Air Force, 1962., 1962), by C. D. Brownfield, D. R. Apodaca, United States. Air Force. Systems Command. Aeronautical Systems Division, United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States, and Northrop Corporation (page images at HathiTrust)
Structural design and analysis of a light-weight laminated composite heat sink for spaceflight PWBs (National Aeronautics and Space Administration, Goddard Space Flight Center, 1997), by Mark S. Fan, W. Lee Niemeyer, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Thermostructural response of advanced reactor cell liners (U.S. Nuclear Regulatory Commission :, 1980), by Charles M. Stone, David K. Gartling, U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research, and Sandia Laboratories (page images at HathiTrust)
Thermo-structural analysis manual (Flight Dynamics Laboratory, Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, 1962), by Republic Aviation Corporation and H. Switzky (page images at HathiTrust)

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