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Libros sobre el tema "Surface Blasts"

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Publicado: 6 de septiembre de 2023

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1

J, Walter Edward, ed. Surface blast design. Englewood Cliffs, N.J: Prentice Hall, 1990.

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2

National Association of Corrosion Engineers., ed. Field measurement of surface profile of abrasive blast-cleaned surfaces using a replica tape. Houston: NACE, 2002.

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3

H, Finlayson M. y United States. National Aeronautics and Space Administration., eds. Evaluation of copper slag blast media for railcar maintenance: Final report. Brigham City, Utah: Morton Thiokol, Inc., Aerospace Group, 1989.

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4

National Association of Corrosion Engineers., ed. Joint surface preparation standard: NACE No. 8/SSPC-SP 14 industrial blast cleaning. Houston: NACE, 1999.

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5

National Association of Corrosion Engineers., ed. Joint surface preparation standard: NACE No. 3/SSPC-SP 6 commercial blast cleaning. Houston: NACE, 1999.

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6

Williams, Marc H. An unsteady lifting surface method for single rotation propellers. Cleveland, Ohio: Lewis Research Center, 1990.

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7

Engineers, National Association of Corrosion. Field measurement of surface profile of abrasive blast cleaned steelsurfaces using a replica tape. Houston: NACE, 1995.

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8

National Association of Corrosion Engineers., ed. Joint surface preparation standard: NACE No. 4/SSPC-SP 7 brush-off blast cleaning. Houston: NACE, 2000.

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9

Connolly, Michael David. Effects of air abrasives on the surface texture of metals. København: Kongelige Danske Kunstakademi, 1986.

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10

Dunn, Mark H. The solution of a singular integral equation arising from a lifting surface theory for rotating blades. [S.l.]: Old Dominion University, 1991.

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11

National Association of Corrosion Engineers., ed. Joint surface preparation standard: NACE No. 2/SSPC-SP 10 near white metal blast cleaning. Houston: NACE, 2000.

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12

E, Siskind D., ed. Comparative study of blasting vibrations from Indiana surface coal mines. Pittsburgh, PA: U.S. Dept. of the Interior, Bureau of Mines, 1988.

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13

Gahagan, Shane G. Pressure-sensitive paint measurements on a rotor disk surface at high speeds. Monterey, Calif: Naval Postgraduate School, 1997.

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14

Siskind, D. E. Low-frequency vibrations produced by surface mine blasting over abandoned underground mines. Pittsburgh, Pa: U.S. Dept. of the Interior, Bureau of Mines, 1987.

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15

Siskind, D. E. Blast vibrations and other potential causes of damage in homes near a large surface coal mine in Indiana. [Washington, DC]: U.S. Dept. of the Interior, Bureau of Mines, 1993.

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16

Kopp, John W. Effects of millisecond-delay intervals on vibration and airblast from surface coal mine blasting. Pittsburgh, Pa: U.S. Dept. of the Interior, Bureau of Mines, 1986.

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17

M, Verdon Joseph y United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Active control of wake/blade-row interaction noise through the use of blade surface actuators. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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18

Laboratory, Construction Engineering Research, ed. A finite difference numerical model for the propagation of finite amplitude acoustical blast waves outdoors over hard and porous surfaces. Champaign, Ill: US Army Corps of Engineers, Construction Engineering Research Laboratory, 1991.

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19

F, Groeneweg J. y Lewis Research Center, eds. Prediction of unsteady blade surface pressures on an advanced propeller at an angle of attack. Cleveland, Ohio: Lewis Research Center, 1989.

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20

Ya, Timofeev I., Shipilov S. D y United States. National Aeronautics and Space Administration., eds. Calculation of the distributed loads on the blades of individual multiblade propellers in axial flow using linear and nonlinear lifting surface theories. Washington, DC: National Aeronautics and Space Administration, 1988.

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21

P, Shreeve Raymond y Lewis Research Center, eds. Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

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22

J, Bruckner R., Smith F. A y United States. National Aeronautics and Space Administration., eds. Application of thin-film thermocouples to localized heat transfer measurements. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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23

Lepicovsky, J. Application of thin-film thermocouples to localized heat transfer measurements. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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24

Lepicovsky, J. Application of thin-film thermocouples to localized heat transfer measurements. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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25

D, Montgomery Matthew, Kousen Kenneth A y United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Development of a linearized unsteady Euler analysis for turbomachinery blade rows. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

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26

D, Montgomery Matthew, Kousen Kenneth A y United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Development of a linearized unsteady Euler analysis for turbomachinery blade rows. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

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27

author, Postal Matthew A., ed. New York Public Library (Stephen A. Schwarzman Building) Interiors, Main Reading Room and Catalog Room (now Rose Main Reading Room and Bill Blass Public Catalog Room), third floor, and the fixtures and interior components of these spaces, which may include but are not limited to the wall surfaces, ceiling surfaces, floor surfaces, murals, decorative plasterwork, metalwork and woodwork, built-in bookcases, balconies and railings, doors and frames, windows and frames, light fixtures, attached furnishings and decorative elements; 476 Fifth Avenue (aka 460-476 FifthAvenue, 1 West 40th Street, 11 West 40th Street, 2 West 42nd Street), Manhattan: Built 1900-1911; Carrère & Hastings, architect. New York]: Landmarks Preservation Commission, 2017.

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28

Joint surface preparation standard: NACE No. 1/SSPC-SP 5 white metal blast cleaning. Houston: NACE, 2000.

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29

National Aeronautics and Space Administration (NASA) Staff. Successful Surface Treatments for Reducing Instabilities in Advanced Nickel-Base Superalloys for Turbine Blades. Independently Published, 2018.

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30

Surface pressure measurements on the blade of an operating Mod-2 wind turbine with and without vortex generators. Washington, D.C: U.S. Dept. of Energy, Conservation and Renewable Energy, Wind/Ocean Technology Division, 1987.

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31

Ruban, Anatoly I. Classical Boundary-Layer Theory. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780199681754.003.0002.

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Chapter 1 discusses the flows that can be described in the framework of Prandtl’s 1904 classical boundary-layer theory, including the Blasius boundary layer on a flat plate and the Falkner–Skan solutions for the boundary layer on a wedge surface. It presents Schlichting’s solution for the laminar jet and Tollmien’s solution for the viscous wake. These are followed by analysis of Chapman’s shear layer performed with the help of Prandtl’s transposition theorem. It also considers the boundary layer on the surface of a fast rotating cylinder with the purpose of linking the circulation around the cylinder with the speed of its rotation. It concludes discussion of the classical boundary-layer theory with analysis of compressible boundary layers, including the interactive boundary layers in hypersonic flows.
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32

Hill, Jason D. Is It Moral to Hold a Racial Identity? Editado por Naomi Zack. Oxford University Press, 2017. http://dx.doi.org/10.1093/oxfordhb/9780190236953.013.39.

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Holding a racial identity is problematic because it turns one into a practicing racist. On the surface this should not be controversial. White supremacists of all stripes, either of the North American variety or the Nazi counterpart, have given us ample evidence of the nefarious nature of strong racial identities, especially when they are wedded to a political ideology that demonizes racial minorities such as blacks or Jews. But we can and should go much further and suggest that the concept of race, simpliciter, is bad. The concomitant practice of holding a racial identity voluntarily and living one’s life as a raciated creature is a form of biological collectivism and racial subjectivism. It matters not whether one is black, white, Indian, or a member of any other designated group; the principle that binds all racial identities together—polylogism—is identical. To self-referentially hold a racial identity is to collude with a great social evil.
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33

Ruban, Anatoly I. Fluid Dynamics. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780199681754.001.0001.

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This is Part 3 of a book series on fluid dynamics. This is designed to give a comprehensive and coherent description of fluid dynamics, starting with chapters on classical theory suitable for an introductory undergraduate lecture courses, and then progressing through more advanced material up to the level of modern research in the field. This book is devoted to high-Reynolds number flows. It begins by analysing the flows that can be described in the framework of Prandtl’s 1904 classical boundary-layer theory. These analyses include the Blasius boundary layer on a flat plate, the Falkner-Skan solutions for the boundary layer on a wedge surface, and other applications of Prandtl’s theory. It then discusses separated flows, and considers first the so-called ‘self-induced separation’ in supersonic flow that was studied in 1969 by Stewartson and Williams, as well as by Neiland, and led to the ‘triple-deck model’. It also presents Sychev’s 1972 theory of the boundary-layer separation in an incompressible fluid flow past a circular cylinder. It discusses the triple-deck flow near the trailing edge of a flat plate first investigated in 1969 by Stewartson and in 1970 by Messiter. It then considers the incipience of the separation at corner points of the body surface in subsonic and supersonic flows. It concludes by covering the Marginal Separation theory, which represents a special version of the triple-deck theory, and describes the formation and bursting of short separation bubbles at the leading edge of a thin aerofoil.
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34

Application of thin-film thermocouples to localized heat transfer measurements. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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