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Shells (Engineering) -- Testing

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• Shells (Engineering)
• Elastic plates and shells -- Testing
• Testing

• Shells (Engineering) -- Testing -- Computer programs
• Blades -- Testing
• Noses (Aircraft) -- Testing
• Tanks -- Testing
• Tubes -- Testing
• Shells (Engineering) -- Aerodynamics -- Testing

• Experimental investigation of the effect of general imperfections on the buckling of cylindrical shells (National Aeronautics and Space Administration]; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1968), by Johann Arbocz, Charles D. Babcock, and California Institute of Technology (page images at HathiTrust; US access only)
• Computer analysis of ring-stiffened shells of revolution (National Aeronautics and Space Administration ;, 1973), by Gerald A. Cohen, Langley Research Center, and Structures Research Associates (page images at HathiTrust)
• Vibration study of a pressurized torus shell (National Aeronautics and Space Administration, 1967), by Peter F. Jordan and Atis A. Liepins (page images at HathiTrust; US access only)
• On the prediction of the vibratory behavior of free-free truncated conical shells (National Aeronautics and Space Administration, 1968), by Eugene C. Naumann and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental and analytical vibration study of thin cylindrical shells with and without longitudinal stiffeners (National Aeronautic and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1968), by John L. Sewall and Eugene C. Naumann (page images at HathiTrust; US access only)
• Automated shell theory for rotating structures (astros) (National Aeronautics and Space Administration [For sale by the National Technical Information Service, Springfield, Va.], 1971), by Byron J. Foster, Jerrell M. Thomas, United States National Aeronautics and Space Administration, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Creep analysis in membrane shells (Polytechnic Institute of Brooklyn, Department of Aerospace Engineering and Applied Mechanics, 1963), by Francis A. Cozzarelli, Sharad A. Patel, United States. Air Force. Office of Aerospace Research, and Polytechnic Institute of Brooklyn. Dept. of Aerospace Engineering and Applied Mechanics (page images at HathiTrust; US access only)

• User document for computer programs for ring-stiffened shells of revolution (National Aeronautics and Space Administration ;, 1973), by Gerald A. Cohen, Langley Research Center, and Structures Research Associates (page images at HathiTrust)

• Development and testing of a pneumatic scraper blade for conveyor belt cleaning (U.S. Dept. of the Interior, Bureau of Mines, 1989), by C. A. Rhoades, T. L. Hebble, and S. G. Grannes (page images at HathiTrust)
• Surface pressure measurements at two tips of a model helicopter rotor in hover (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by R. B. Gray, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Development and testing of a pneumatic scraper blade for conveyor belt cleaning (U.S. Dept. of the Interior, Bureau of Mines, 1989), by C. A. Rhoades, T. L. Hebble, and S. G. Grannes (page images at HathiTrust)

• Effect of hole geometry and electric-discharge machining (EDM) on airflow rates through small-diameter holes in turbine-blade material (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980), by Steven A. Hippensteele and Reeves P. Cochran (page images at HathiTrust)
• Flow visualization of discrete-hole film cooling with a spanwise injection over a cylinder (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Louis M. Russell, Lewis Research Center, 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)
• Turbine engine diagnostics system study (FAA Technical Center ;, 1991), by Barbara K. McQuiston, Ronald L. De Hoff, Inc Systems Control Technology, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)

• Fluctuating pressures on fan blades of a turbofan engine : flight test investigation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by James A. Schoenster and Langley Research Center (page images at HathiTrust)

• Investigation of an impulse axial-flow compressor rotor over a range of blade angles (National Advisory Committee for Aeronautics, 1950), by Wallace M. Schulze, Willard R. Westphal, John R. Erwin, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Design, over-all performance and stall characteristics (National Advisory Committee for Aeronautics, 1954), by George W. Lewis, G. K. Serovy, Francis C. Schwenk, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)

• Off-design correlation for losses due to part-span dampers on transonic rotors. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by William B. Roberts, Donald M. Sandercock, James E. Crouse, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Overall and blade-element performance of a 1.20-pressure-ratio fan stage at design blade setting angle (National Aeronautics and Space Administration ;, 1974), by George W. Lewis, Edward R. Tysl, and Lewis Research Center (page images at HathiTrust)
• Overall and blade element performance of a 1.20-pressure-ratio fan stage with rotor blades reset -5 ̊ (U.S. National Aeronautics and Space Administration ;, 1976), by George W. Lewis, Royce D. Moore, Walter Martin Osborn, and Lewis Research Center (page images at HathiTrust)
• Overall and blade element performance of a 1.20 pressure ratio fan stage with rotor blades reset -7 ̊ (U.S. National Aeronautics and Space Administration ;, 1976), by George W. Lewis, George Kovich, and Lewis Research Center (page images at HathiTrust)

• Fluctuating pressures on fan blades of a turbofan engine : static and wind-tunnel investigations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by James A. Schonester, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)

• Stagnation region gas film cooling : spanwise angled injection from multiple rows of holes (National Aeronautics and Space Administration ;, 1981), by D. W. Luckey, M. R. L'Ecuyer, Lewis Research Center, Purdue University. Thermal Sciences and Propulsion Center, United States National Aeronautics and Space Administration, and United States. Office of Naval Research (page images at HathiTrust)

• An evaluation of three oxidation-resistant alloy claddings for IN 100 and WI 52 superalloys (National Aeronautics and Space Administration ;, 1969), by Michael A. Gedwill, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• A nickel-base alloy, NASA WAZ-16, with potential for gas turbine stator vane application (National Aeronautics and Space Administration ;, 1974), by William J. Waters, John C. Freche, and Lewis Research Center (page images at HathiTrust)
• Factors affecting miniature Izod impact strength of tungsten-fiber-metal-matrix composites (National Aeronautics and Space Administration ;, 1973), by Edward A. Winsa, Donald W. Petrasek, and Lewis Research Center (page images at HathiTrust)
• Stress-rupture strength and microstructural stability of tungsten-hafnium-carbon-wire-reinforced superalloy composites (National Aeronautics and Space Administration ;, 1974), by Donald W. Petrasek, Robert A. Sigorelli, and Lewis Research Center (page images at HathiTrust)

• Nonlinear, three-dimensional finite-element analysis of air-cooled gas turbine blades (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Albert Kaufman, Raymond E. Gaugler, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Durability of zirconia thermal-barrier ceramic coatings on air-cooled turbine blades in cyclic jet engine operation (National Aeronautics and Space Administration ;, 1976), by Lewis Research Center, Curt H. Liebert, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance of two tangential jet blades (National Aeronautics and Space Administration ;, 1970), by James L. Bettner, Lewis Research Center, and General Motors Company (page images at HathiTrust)
• Performance evaluation of modified jet-flap rotor blade. (National Aeronautics and Space Administration, 1971), by H. G. Lueders, United States National Aeronautics and Space Administration, Lewis Research Center, and General Motors Corporation (page images at HathiTrust)
• Performance evaluation of plain rotor blade with plow type vortex generators (National Aeronautics and Space Administration, 1969), by H. G. Lueders (page images at HathiTrust)
• Experimental investigation of advanced concepts to increase turbine blade loading : II. performance evaluation of plain rotor blade (National Aeronautics and Space Administration, 1968), by H. G. Lueders (page images at HathiTrust; US access only)
• Performance evaluation of jet-flap rotor blade (National Aeronautics and Space Administration, 1970), by H. G. Lueders, United States National Aeronautics and Space Administration, Lewis Research Center, and General Motors Corporation (page images at HathiTrust)
• Performance evaluation of modified tandem rotor blade (National Aeronautics and Space Administration, 1970), by H. G. Lueders, United States National Aeronautics and Space Administration, Lewis Research Center, and General Motors Corporation (page images at HathiTrust)
• Performance evaluation of a two-stage turbine designed for a ratio of blade speed to jet speed of 0.146 (National Aeronautics and Space Administration, 1960), by Milton G. Kofskey, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Fabrication and endurance of air-cooled strut-supported turbine blades with struts cast of X-40 alloy (National Advisory Committee for Aeronautics, 1956), by Eugene F. Schum, Robert E. Oldrieve, Francis S. Stepka, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Analytical and experimental investigation of a forced-convection air-cooled internal strut-supported turbine blade (National Advisory Committee for Aeronautics, 1954), by Eugene F. Schum, Francis S. Stepka, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)

• Side forces on a tangent ogive forebody with a fineness ratio of 3.5 at high angles of attack and Mach numbers from 0.1 to 0.7 (National Aeronautics and Space Administration ;, 1977), by Earl R. Keener and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Subsonic wind-tunnel investigation of errors indicated by total-pressure tubes in the flow field of a body simulating the nose of the X-15 research airplane. William J. Alford Jr. (National Aeronautics and Space Administration :, 1962), by William J. Alford and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Laminar boundary-layer separation induced by flares on cylinders with highly cooled boundary layers at a Mach number of 15 (National Aeronautics and Space Administration :, 1965), by Donald M. Kuehn and Ames Research Center (page images at HathiTrust)
• Performance of a translating-double-cone axisymmetric inlet with cowl bypass at mach number from 2.0 to 3.5 (National Advisory Committee for Aeronautics, 1957), by James F. Connors, GeorgeA. Wise, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Metallurgical analysis of ablated aluminum alloy hemispheres (Polytechnic Institute of Brooklyn, Department of Aerospace Engineering and Applied Mechanics, 1962), by G. J. Fischer, R. Maciag, and Polytechnic Institute of Brooklyn. Dept. of Aerospace Engineering and Applied Mechanics (page images at HathiTrust; US access only)

• Stabilization/solidification of CERCLA and RCRA wastes : physical tests, chemical testing procedures, technology screening, and field activities. (Center for Environmental Research Information :, 1989), by Center for Environmental Research Information (U.S.) and Risk Reduction Engineering Laboratory (U.S.) (page images at HathiTrust)
• Volumetric tank testing : an overview (Center for Environmental Research Information, Office of Research and Development, U.S. Environmental Protection Agency, 1989), by J. W. Maresca, Monique Seibel, and Center for Environmental Research Information (U.S.) (page images at HathiTrust)
• Contoured tank outlets for draining of cylindrical tanks in low-gravity environment (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Eugene P. Symons, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)

• Interim report on the hydrostatic destructive testing of Zircaloy-2 pressure tubing (U.S. Atomic Energy Commission, 1959), by V. E. Kahle, United States. National Bureau of Standards, United States. Department of Energy. Office of Fusion Energy, United States. National Bureau of Standards. Fracture and Deformation Division, 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)
• Tests of flexible gas tubing (U.S. Dept. of Commerce, Bureau of Standards :, 1919), by R. S. McBride, Ellsworth Francisco, Walter Matho Berry, and United States. National Bureau of Standards (page images at HathiTrust)
• Evaluation of tantalum/316 stainless steel bimetallic tubing (National Aeronautics and Space Administration ;, 1970), by J. N. Kass, D. R. Stoner, Lewis Research Center, and Westinghouse Electric Corporation. Astronuclear Laboratory (page images at HathiTrust)
• Durability tests on pyrex raschig rings (Denver, Colorado : Dow Chemical Company, Rocky Flats Plant ; Washington, D.C : Office of Technical Services, Department of Commerce, 1962., 1962), by C. L. Schuske, H. W. King, U.S. Atomic Energy Commission, and Dow Chemical Company. Rocky Flats Division (page images at HathiTrust)
• Fabrication of the Plutonium Recycle Test Reactor zircaloy-2 high pressure process tubes (Hanford Atomic Products Operation, 1959), by R. L. Knecht, General Electric Company, U.S. Atomic Energy Commission, and Hanford Atomic Products Operation (page images at HathiTrust)
• Stress corrosion cracking of inconel 600 tubing in deaerated high temperature water (Upton, New York : Brookhaven National Laboratory, Dept. of Nuclear Energy, Corrosion Science Group, 1979., 1979), by T. S. Bulischeck, Y. S. Park, Daniel Van Rooyen, U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research, and Brookhaven National Laboratory. Department of Nuclear Energy. Corrosion Science Group (page images at HathiTrust)

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