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Sensitivity analysis of the C-130 sensor deployment system arm using finite element methodsFeragotti, Lawrence Anthony. January 1900 (has links)
Thesis (M.S.)--West Virginia University, 2004. / Title from document title page. Document formatted into pages; contains xii, 125 p. : ill. (some col.). Includes abstract. Includes bibliographical references (p. 43-44).
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Aircraft intercom system design for Project OculusWilhelm, Jay Paul. January 2005 (has links)
Thesis (M.S.)--West Virginia University, 2005. / Title from document title page. Document formatted into pages; contains ix, 89 p. : ill. (some col.). Includes abstract. Includes bibliographical references (p. 58-59).
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Design validation methodology development for an aircraft sensor deployment systemWowczuk, Zenovy S. January 2008 (has links)
Thesis (Ph. D.)--West Virginia University, 2008. / Title from document title page. Document formatted into pages; contains xv, 294 p. : ill. (some col.). Includes abstract. Includes bibliographical references.
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A service life analysis of U.S. Coast Guard C-130 aircraftDuff, Jonathan B. January 2003 (has links)
Thesis (M.S.)--Air Force Institute of Technology, 2003. / Title from title screen (viewed May 10, 2004). "March 2003." Vita. "AFIT/GAQ/ENS/03-02." "ADA413132"--URL. Includes bibliographical references (leaves 132-135). Also issued in paper format.
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Design of a standardized sensor platform for a C-130 aircraftWowczuk, Zenovy S. January 1900 (has links)
Thesis (M.S.)--West Virginia University, 2004. / Title from document title page. Document formatted into pages; contains xi, 99 p. : ill. (some col.). Includes abstract. Includes bibliographical references (p. 58-59).
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Control system design for a C-130 ro-ro sensor deployment platformHayes, Robert Paul. January 2004 (has links)
Thesis (M.S.)--West Virginia University, 2004. / Title from document title page. Document formatted into pages; contains xi, 190 p. : ill. (some col.). Vita. Includes abstract. Includes bibliographical references (p. 116-119).
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Dynamic modal analysis and optimization of C-130 Project Oculus' mechanical arm/pod sensor deployment system using the finite element methodNaternicola, Adam C., January 1900 (has links)
Thesis (M.S.)--West Virginia University, 2004. / Title from document title page. Document formatted into pages; contains xvii, 142 p. : ill. (some col.). Vita. Includes abstract. Includes bibliographical references (p. 80-81).
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Design of a quick-release mechanism for a C-130 aircraft sensor platformLucey, Seth D. January 1900 (has links)
Thesis (M.S.)--West Virginia University, 2006. / Title from document title page. Document formatted into pages; contains viii, 73 p. : ill. (some col.). Includes abstract. Includes bibliographical references (p. 56-58).
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Investigation of the Impact of Turboprop Propulsion on Fuel Efficiency and Economic FeasibilityAntcliff, Kevin Richard 02 October 2014 (has links)
This study explored a 130-passenger advanced turboprop commercial airliner with the purposes of economic feasibility and energy efficiency. A baseline vehicle and a derivative vehicle were researched and analyzed in detail. Based on the findings of this analysis, an advanced future airliner was designed. For the advanced airliner, advanced technologies were suggested and projections of these technology benefits were implemented. Detailed performance analysis was conducted for all three aircraft. The energy efficiency of each vehicle was compared to current and future N+3 aircraft. Lastly, cost analysis was performed to observe the impact of these energy savings.
The three existing and future concepts evaluated were: 1) Bombardier 80- passenger Q400 baseline, 2) An expanded 130-passenger Bombardier Q400 termed the Q400XL, and 3) an N+3 advanced 130-passenger turboprop airliner termed the N+3 Airliner. The N+3 Airliner was compared to the SUGAR High, a Boeing/NASA N+3 aircraft, in both fuel efficiency and economic feasibility. The N+3 Airliner was 22 percent more energy efficient. At current oil prices, the N+3 Airliner had nearly identical operating cost. However, at two times current oil prices, the N+3 Airliner has a slight advantage economically. Therefore, as long as the price of oil is above 2011 oil prices, $3.03 per barrel, the N+3 Airliner will be an economically viable option. / Ph. D.
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A rotational arm connection point design for a C-130 aircraft standardized sensor platformWilliams, Kenneth A. January 2006 (has links)
Thesis (M.S.)--West Virginia University, 2006. / Title from document title page. Document formatted into pages; contains viii, 77 p. : ill. (some col.). Includes abstract. Includes bibliographical references (p. 58-59).
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