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Tensile And Compressive Stress Strain Properties Of Some High Strength Sheet Alloys At Elevated Temperatures
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Book Synopsis Tensile and Compressive Stress-strain Properties of Some High-strength Sheet Alloys at Elevated Temperatures by : Philip J. Hughes
Download or read book Tensile and Compressive Stress-strain Properties of Some High-strength Sheet Alloys at Elevated Temperatures written by Philip J. Hughes and published by . This book was released on 1954 with total page 672 pages. Available in PDF, EPUB and Kindle. Book excerpt: Representative tensile and compressive stress-strain curves are give for each material at the test temperatures. The variations of the tensile and compressive properties with temperature is shown for specimens tested parallel and transverse to the rolling direction of the materials. Secant and tangent moduli, obtained from the compressive data, are included.
Book Synopsis Mechanical Properties of Selected Alloys at Elevated Temperatures by : Bell Aircraft Corporation. Engineering and Research Laboratories
Download or read book Mechanical Properties of Selected Alloys at Elevated Temperatures written by Bell Aircraft Corporation. Engineering and Research Laboratories and published by . This book was released on 1960 with total page 284 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Determination of the Effects of Elevated Temperature Materials Properties of Several High Temperature Alloys by : Meyer Marshall Lemcoe
Download or read book Determination of the Effects of Elevated Temperature Materials Properties of Several High Temperature Alloys written by Meyer Marshall Lemcoe and published by . This book was released on 1962 with total page 408 pages. Available in PDF, EPUB and Kindle. Book excerpt: This investigation was conducted to determine mechanical properties of several high performance alloys at room and elevated temperatures. The effects of temperature (up to 1900 F) and exposure (up to 1000 hours) at temperature on the tensile, compressive, bearing and shear properties were determined from measured stress-strain information in both the elastic and plastic range. The following materials were considered: 301 extra hard stainless steel; Ph157Mo(TH 1050); AM 355; Rene 41; and N-155. All material was from 0.050-inch sheet, except the material for the 1/8-inch diameter shear pins, which were fabricated from 1/4-inch plate. Heat treatment was in accordance with existing specifications for the materials, or other procedures approved by ASD to develop the optimum strength properties. Descriptions of the test specimens, equipment, and procedures are included. Test results are reported in tables and in curves showing the effects of temperature and time on the various mechanical properties.
Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page 606 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Moderately High Strain Rates on the Tensile Properties of Metals by : D. P. Moon
Download or read book Effects of Moderately High Strain Rates on the Tensile Properties of Metals written by D. P. Moon and published by . This book was released on 1961 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Tensile Properties and Sheet-bending Fatigue Properties of Some Refractory Metals at Room Temperature by : Lee R. Foster
Download or read book Tensile Properties and Sheet-bending Fatigue Properties of Some Refractory Metals at Room Temperature written by Lee R. Foster and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results of tensile stress-strain tests and completely reversed sheet-bending fatigue tests conducted at room temperature on unnotched sheet specimens of Ta-lOW tantalum alloy, D-3l niobium alloy, pure tungsten, and Mo-0.5Ti molybdenum alloy are presented. Fatigue data from tests on similar specimens of 2024-T3 aluminum alloy and 17-7 PH stainless steel are compared with previous data from axial-load tests on larger specimens of these materials to determine whether the small size of the specimens used in this investigation produces representative results. Comparisons of the various materials on the basis of applied-stress- ultimate-strength and strength-density ratio also are presented.
Download or read book Nuclear Science Abstracts written by and published by . This book was released on with total page 1146 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Note written by and published by . This book was released on 1955 with total page 420 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis General Theory of Wave-drag Reduction for Combinations Employing Quasi-cylindrical Bodies with an Application to Swept-wing and Body Combinations by : Jack N. Nielsen
Download or read book General Theory of Wave-drag Reduction for Combinations Employing Quasi-cylindrical Bodies with an Application to Swept-wing and Body Combinations written by Jack N. Nielsen and published by . This book was released on 1956 with total page 676 pages. Available in PDF, EPUB and Kindle. Book excerpt: The wing-body interference theory of NACA TN 2677 applied to symmetrical wings in combination with quasi-cylindrical bodies permits the direct calculation of pressure-distribution changes produced by body shape changes. This theory is used to determine the relative magnitued of the wave-drag reduction produced by changes in cylinder cross-sectional area and that produced changes in cross-sectional shape (without change in area). The body distortion is expressed as a Fourier series, and an integral equation is derived for the body shape for minimum drag for each Fourier component. Thus the wave-drag reductions for the various Fourier harmonics are independent and additive.
Download or read book NASA Technical Note written by and published by . This book was released on 1961 with total page 462 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Index of NACA Technical Publications by : United States. National Advisory Committee for Aeronautics
Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1955 with total page 1338 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by :
Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by and published by . This book was released on 1949 with total page 664 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1960 with total page 1006 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Selected Short-time Tensile and Creep Data Obtained Under Conditions of Rapid Hearting by : Donald P. Moon
Download or read book Selected Short-time Tensile and Creep Data Obtained Under Conditions of Rapid Hearting written by Donald P. Moon and published by . This book was released on 1960 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Attenuation of Strong Shock Waves in a Shock Tube with Hydrogen and Helium as Driver Gases by : Jim J. Jones
Download or read book Experimental Investigation of Attenuation of Strong Shock Waves in a Shock Tube with Hydrogen and Helium as Driver Gases written by Jim J. Jones and published by . This book was released on 1957 with total page 716 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation has been made of the attenuation of strong shock waves in air in a shock tube. Time-history measurements were made of the static pressure at several stations in the wall of the tube. The internal diameter of the tube is 3.75 inches. shock-wave-velocity data were taken for a distance along the tube of about 120 feet.
Book Synopsis Aerospace Structural Metals Handbook by :
Download or read book Aerospace Structural Metals Handbook written by and published by . This book was released on 1989 with total page 938 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Tensile Stress-strain Properties of 17-7 PH and AM Stainless-steel Sheet at Elevated Temperatures by : Ivo M. Kurg
Download or read book Tensile Stress-strain Properties of 17-7 PH and AM Stainless-steel Sheet at Elevated Temperatures written by Ivo M. Kurg and published by . This book was released on 1957 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tensile stress-strain test results are presented for 17-7 PH stainless-steel sheet in the Conditions TN 1,050 and for AM 350 stainless-steel sheet in the double-aged condition for temperatures from room temperatures to 1,300 degrees F. Stress-strain curves and data for yield and ultimate stresses, Young's modulus, and elongation are given in tabular and graphical form. A comparison is made between the tensile properties and the compressive properties of NACA Technical Note 4074.