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Books on the topic 'Flex engine'

Author: Grafiati
Published: 4 June 2021
Last updated: 1 February 2022

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1

Meldrum, Jay. Clean Snowmobile Challenge - 2: The Revival of the 2-stroke Engine and Studying Flex Fuel Engines. Warrendale, PA: SAE International, 2017. http://dx.doi.org/10.4271/srp-003.

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2

Liebert, Curt H. Heat flux measurement in SSME turbine blade tester. [Washington, DC]: National Aeronautics and Space Administration, 1990.

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3

Kopp, Robert William. Determination of the velocity, density, mass flux and enthalpy profiles for very high temperature arc jet nozzle flow. Monterey, Calif: Naval Postgraduate School, 1989.

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4

Jankovsky, Robert S. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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5

High-frequency data observations from space shuttle main engine low pressure fuel turbopump discharge duct flex joint tripod failure investigation. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1991.

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6

A, Farr R., and George C. Marshall Space Flight Center., eds. High-frequency data observations from space shuttle main engine low pressure fuel turbopump discharge duct flex joint tripod failure investigation. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1991.

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7

A, Farr R., and George C. Marshall Space Flight Center., eds. High-frequency data observations from space shuttle main engine low pressure fuel turbopump discharge duct flex joint tripod failure investigation. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1991.

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8

J, Gladden Herbert, and United States. National Aeronautics and Space Administration., eds. A unique high heat flux facility for testing hypersonic engine components. [Washington, DC]: National Aeronautics and Space Administration, 1990.

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9

United States. National Aeronautics and Space Administration., ed. Research instrumentation for hot section components of turbine engines. [Washington, D.C: National Aeronautics and Space Administration, 1986.

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10

Hypersonic engine component experiments in a high heat flux, supersonic flow environment. [Cleveland, Ohio]: NASA, [Lewis Research Center], 1993.

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11

E, Melis Matthew, and United States. National Aeronautics and Space Administration., eds. Hypersonic engine leading edge experiments in a high heat flux, supersonic flow environment. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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12

F, Barrows Richard, United States. National Aeronautics and Space Administration., and United States. Dept. of Energy. Office of Vehicle and Engine Research and Development., eds. Prototype thin-film thermocouple/heat-flux sensor for a ceramic-insulated diesel engine. Washington, D.C: U.S. Dept. of Energy, Conservation and Renewable Energy, Office of Vehicle and Engine R&D, 1988.

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13

Prototype thin-film thermocouple/heat-flux sensor for a ceramic-insulated diesel engine. Washington, D.C: U.S. Dept. of Energy, Conservation and Renewable Energy, Office of Vehicle and Engine R&D, 1988.

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14

F, Barrows Richard, United States. National Aeronautics and Space Administration., and United States. Dept. of Energy. Office of Vehicle and Engine Research and Development., eds. Prototype thin-film thermocouple/heat-flux sensor for a ceramic-insulated diesel engine. Washington, D.C: U.S. Dept. of Energy, Conservation and Renewable Energy, Office of Vehicle and Engine R&D, 1988.

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15

Thermal modelling of various thermal barrier coatings in a high heat flux rocket engine. [Washington, DC: National Aeronautics and Space Administration, 1990.

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16

United States. National Aeronautics and Space Administration., ed. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket engine calorimeter heat transfer measurements and analysis. [Washington, D.C.]: National Aeronautics and Space Administration, 1997.

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17

Peek, Chester L. Flying with 40 horses: A history of the Continental A-40 aircraft engine and the planes it flew. Three Peaks Pub, 2001.

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18

United States. National Aeronautics and Space Administration., ed. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket engine calorimeter heat transfer measurements and analysis. [Washington, D.C.]: National Aeronautics and Space Administration, 1997.

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19

S, Zakany James, and United States. National Aeronautics and Space Administration., eds. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket heat transfer and combustion measurements. [Washington, D.C: National Aeronautics and Space Administration, 1996.

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20

S, Zakany James, and United States. National Aeronautics and Space Administration., eds. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket combustion experiments. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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21

D, Smith Timothy, Pavli Albert J, and NASA Glenn Research Center, eds. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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22

D, Smith Timothy, Pavli Albert J, and NASA Glenn Research Center, eds. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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23

D, Smith Timothy, Pavli Albert J, and NASA Glenn Research Center, eds. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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24

High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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25

Tyler, Amanda L. Suspension. Oxford University Press, 2017. http://dx.doi.org/10.1093/oso/9780199856664.003.0003.

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The crowning of William and Mary and the Glorious Revolution witnessed the restoration of a Protestant monarchy, the continued rise of parliamentary supremacy, and the adoption of the Declaration of Rights. It did not, however, bring a settled peace. Despite their king having fled, James II’s supporters remained eager to engineer his return. It was to defeat the plotting of the Jacobites that Parliament invented suspension for setting aside the very protections for which it had provided in the Habeas Corpus Act of 1679. This chapter details the many suspensions that followed during the Jacobite Wars and war with France, while also detailing how bills of attainder similarly empowered Parliament to work around the constraints of the Habeas Corpus Act. The chapter concludes by highlighting the important legal distinctions drawn in English law during this period between prisoners of war and traitors.
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26

United States. National Aeronautics and Space Administration., ed. Simplified numerical description of SPT operation. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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27

S, Zakany James, and United States. National Aeronautics and Space Administration., eds. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket heat transfer and combustion measurements. [Washington, D.C: National Aeronautics and Space Administration, 1996.

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28

S, Zakany James, and United States. National Aeronautics and Space Administration., eds. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket combustion experiments. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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29

Wheatley, Pat, and Charlotte Dunn. Demetrius the Besieger. Oxford University Press, 2020. http://dx.doi.org/10.1093/oso/9780198836049.001.0001.

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Demetrius the Besieger is a historical and historiographical biography of Demetrius Poliorcetes ‘The Besieger of Cities’ (336–282 BC), an outstanding, yet enigmatic figure who presided over the disintegration of Alexander the Great’s empire after 323 BC. His campaigns, initiatives, and personal life bestride the opening forty years of the so-called ‘Hellenistic’ age, and are pivotal in its formation. Son of Antigonus Monophthalmus ‘The One-Eyed’, who fought alongside Alexander, Demetrius is the most fascinating and high profile of the Diadochoi, or Successors to Alexander the Great, and he became the first of the Hellenistic kings. This work provides a detailed account of Demetrius’ life set in the historical context of the chaotic period following Alexander’s unexpected death. It examines his career as a general, a king, and a legendary womanizer, presenting both the triumphs and disasters experienced by this remarkable individual. Demetrius was especially famous for his spectacular siege operations against enemy cities, and gained his unique nickname from his innovation in building gigantic siege engines, which were engineering wonders of the ancient world. However, his life was a paradox, with his fortunes oscillating wildly between successful and catastrophic ventures. His intrinsic qualities were hotly debated by the ancients, and remain controversial to this day. What is indisputable is that his endeavours dominated a formative period marked by great flux and enormous change, and his dazzling persona supplies a lens through which we can understand Hellenistic history.
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30

Cox, Peter, and Till Koglin, eds. The Politics of Cycling Infrastructure. Policy Press, 2020. http://dx.doi.org/10.1332/policypress/9781447345152.001.0001.

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Academic texts on cycling research are expanding rapidly. A dominant theme among these is the use of infrastructure measures to assist promotion of cycling as part of a movement towards sustainable mobility. Physical infrastructure is currently posited as the primary key to unlock cycling’s potential as a primary mode of sustainable transport. Individual studies rarely stand together to be read back to back, in order to allow comparison between them. The privilege of academic conferences is that they allow the attendee to compare and contrast different academic agendas and concerns of researchers, and to engage in conversation between them. This volume provides a comparative assessment of existing and historic struggles over cycling infrastructure. The aim of this volume is to bring a selection of those parallel voices together and to initiate that dialogue for a wider audience. It is argued that planning is one element of the operation, but what results is often very different from even the most comprehensive strategic imagination. Underlying this chaos however, is a lurking sense that the broader lessons of infrastructure provision for cycling needs to be connected with the political analyses of infrastructuring that derive from wider studies. The book concludes that infrastructures are in constantly in flux, contentious and contended. Furthermore, it concludes that politics is also embodied; lived out in the spaces of mundane and everyday travel.
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31

Note, Lineman. Wind Blew the Shit Flew and Out Came the Line Crew Composition Notebook: Great Notebook Gifts for Electrical Engineer, Lineman and Electrician, Composition Notebook 7. 5 X9. 25 , 120 Wide Ruled Pages Journal Diary. Independently Published, 2020.

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