URL: https://mediatum.ub.tum.de/doc/1283437/1283437.pdf
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<< /S /GoTo /D (chapter.1) >>
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(Introduction)
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<< /S /GoTo /D (chapter.2) >>
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8 0 obj
(The Propcraft P-420 aircraft concept)
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<< /S /GoTo /D (section.2.1) >>
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(Development of the initial aircraft concept)
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<< /S /GoTo /D (subsection.2.1.1) >>
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(Market analysis and requirements)
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<< /S /GoTo /D (subsection.2.1.2) >>
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20 0 obj
(Summary of the P-420/A concept)
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<< /S /GoTo /D (subsection.2.1.3) >>
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(Design mission)
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<< /S /GoTo /D (section.2.2) >>
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(Development of an integrated design tool and modification of the P-420/A)
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<< /S /GoTo /D (subsection.2.2.1) >>
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32 0 obj
(Introduction of the IDT)
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<< /S /GoTo /D (subsection.2.2.2) >>
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36 0 obj
(The P-420/B)
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<< /S /GoTo /D (section.2.3) >>
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(Trade studies)
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<< /S /GoTo /D (section.2.4) >>
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(Analysis and modification of the P-420/B and the IDT)
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<< /S /GoTo /D (subsection.2.4.1) >>
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(Propeller mass estimation)
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<< /S /GoTo /D (subsection.2.4.2) >>
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(Taxi power settings)
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<< /S /GoTo /D (subsection.2.4.3) >>
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(Limitation of the ROCD)
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<< /S /GoTo /D (subsection.2.4.4) >>
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(Usability of the IDT)
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<< /S /GoTo /D (section.2.5) >>
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(Definition of requirements)
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<< /S /GoTo /D (chapter.3) >>
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(Theory)
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<< /S /GoTo /D (section.3.1) >>
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(Point mass model and total energy method)
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<< /S /GoTo /D (section.3.2) >>
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(Jet engine thrust)
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<< /S /GoTo /D (section.3.3) >>
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(Specific Fuel Consumption \(SFC\))
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<< /S /GoTo /D (section.3.4) >>
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(Takeoff Climb Gradient Requirements)
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<< /S /GoTo /D (chapter.4) >>
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(Integration of turbofan engines into the P-420 aircraft concept)
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<< /S /GoTo /D (section.4.1) >>
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(Motivation)
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<< /S /GoTo /D (section.4.2) >>
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(Advantages and disadvantages of turbofan engines compared to turboprop engines)
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<< /S /GoTo /D (subsection.4.2.1) >>
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(Mass)
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<< /S /GoTo /D (subsection.4.2.2) >>
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(Aerodynamics)
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<< /S /GoTo /D (subsection.4.2.3) >>
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(Thrust characteristics and flight performance)
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<< /S /GoTo /D (subsection.4.2.4) >>
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(Fuel consumption)
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<< /S /GoTo /D (subsection.4.2.5) >>
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(Noise)
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<< /S /GoTo /D (subsection.4.2.6) >>
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(Engine availability)
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<< /S /GoTo /D (subsection.4.2.7) >>
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(Operational aspects)
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<< /S /GoTo /D (section.4.3) >>
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(Modification of the IDT)
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<< /S /GoTo /D (subsection.4.3.1) >>
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(Mass)
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<< /S /GoTo /D (subsection.4.3.2) >>
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(Aerodynamics)
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<< /S /GoTo /D (subsection.4.3.3) >>
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(Turbofan engine parameter calculation)
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<< /S /GoTo /D (section.4.4) >>
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(Turbofan engine choice)
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<< /S /GoTo /D (subsection.4.4.1) >>
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(General Electric GEnx-1B76)
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<< /S /GoTo /D (subsection.4.4.2) >>
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(Pratt \046 Whitney PW1127G)
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<< /S /GoTo /D (section.4.5) >>
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156 0 obj
(Analysis of aircraft performance)
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<< /S /GoTo /D (subsection.4.5.1) >>
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(Mass)
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<< /S /GoTo /D (subsection.4.5.2) >>
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(Aerodynamics)
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<< /S /GoTo /D (subsection.4.5.3) >>
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(Engine Characteristics)
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<< /S /GoTo /D (subsection.4.5.4) >>
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172 0 obj
(Performance)
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<< /S /GoTo /D (subsection.4.5.5) >>
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176 0 obj
(Fuel consumption and payload-range characteristics)
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<< /S /GoTo /D (subsection.4.5.6) >>
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(Discussion of engine number)
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<< /S /GoTo /D (chapter.5) >>
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(Fuel efficiency analysis)
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<< /S /GoTo /D (section.5.1) >>
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(Problem statement)
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<< /S /GoTo /D (section.5.2) >>
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192 0 obj
(Base of Aircraft Data \(BADA\))
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<< /S /GoTo /D (subsection.5.2.1) >>
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(Limitations of BADA)
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<< /S /GoTo /D (section.5.3) >>
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(Fuel Consumption and Emissions Calculation Tool \(FCECT\))
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<< /S /GoTo /D (subsection.5.3.1) >>
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(Single Mission Calculator)
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<< /S /GoTo /D (subsection.5.3.2) >>
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(Modifications to the FCECT)
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<< /S /GoTo /D (section.5.4) >>
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(Derivation of BADA coefficients)
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<< /S /GoTo /D (subsection.5.4.1) >>
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(OPF)
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<< /S /GoTo /D (subsection.5.4.2) >>
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(APF)
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<< /S /GoTo /D (subsection.5.4.3) >>
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(SYNONYM\137ALL.LST file)
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<< /S /GoTo /D (section.5.5) >>
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228 0 obj
(Analysis)
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<< /S /GoTo /D (subsection.5.5.1) >>
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232 0 obj
(Competitor aircraft)
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<< /S /GoTo /D (subsection.5.5.2) >>
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(Mission parameters and boundary conditions)
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<< /S /GoTo /D (section.5.6) >>
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240 0 obj
(Results)
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<< /S /GoTo /D (subsection.5.6.1) >>
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244 0 obj
(420 PAX and 5 t cargo)
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<< /S /GoTo /D (subsection.5.6.2) >>
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248 0 obj
(315 PAX and 3.75 t cargo)
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<< /S /GoTo /D (subsection.5.6.3) >>
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252 0 obj
(P-420 design mission)
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<< /S /GoTo /D (subsection.5.6.4) >>
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256 0 obj
(P-420 versions)
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<< /S /GoTo /D (subsection.5.6.5) >>
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260 0 obj
(Summary)
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<< /S /GoTo /D (chapter.6) >>
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264 0 obj
(Sensitivity Analysis)
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<< /S /GoTo /D (section.6.1) >>
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268 0 obj
(Identification of sensitivities)
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<< /S /GoTo /D (subsection.6.1.1) >>
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(Taxi times)
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<< /S /GoTo /D (subsection.6.1.2) >>
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(Initial cruise altitude)
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<< /S /GoTo /D (subsection.6.1.3) >>
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(Airspeed)
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<< /S /GoTo /D (section.6.2) >>
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284 0 obj
(Results)
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<< /S /GoTo /D (subsection.6.2.1) >>
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(Taxi times)
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<< /S /GoTo /D (subsection.6.2.2) >>
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(Initial cruise altitude)
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<< /S /GoTo /D (subsection.6.2.3) >>
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(Airspeed)
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<< /S /GoTo /D (subsection.6.2.4) >>
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(Conclusion)
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<< /S /GoTo /D (chapter.7) >>
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304 0 obj
(Integration of the Integrated Design Tool into the Aircraft DEsign BOx)
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<< /S /GoTo /D (section.7.1) >>
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308 0 obj
(Introduction to the ADEBO)
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<< /S /GoTo /D (section.7.2) >>
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(P-420 Configuration)
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<< /S /GoTo /D (section.7.3) >>
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(Input and output wrapper)
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<< /S /GoTo /D (section.7.4) >>
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(Workflow)
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<< /S /GoTo /D (section.7.5) >>
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324 0 obj
(Conclusion)
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<< /S /GoTo /D (chapter.8) >>
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328 0 obj
(Outlook and conclusion)
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<< /S /GoTo /D (chapter.8) >>
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331 0 obj
(Bibliography)
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<< /S /GoTo /D (appendix.A) >>
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(Appendix)
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<< /S /GoTo /D (section.A.1) >>
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339 0 obj
(APF)
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<< /S /GoTo /D (subsection.A.1.1) >>
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343 0 obj
(P-420/B APF file)
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<< /S /GoTo /D (subsection.A.1.2) >>
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347 0 obj
(P-420/C APF file)
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<< /S /GoTo /D (subsection.A.1.3) >>
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351 0 obj
(P-420/G APF file)
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<< /S /GoTo /D (subsection.A.1.4) >>
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(P-420/T APF file)
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356 0 obj
<< /S /GoTo /D (section.A.2) >>
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359 0 obj
(OPF)
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<< /S /GoTo /D (subsection.A.2.1) >>
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(P-420/B OPF file)
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<< /S /GoTo /D (subsection.A.2.2) >>
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367 0 obj
(P-420/C OPF file)
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<< /S /GoTo /D (subsection.A.2.3) >>
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371 0 obj
(P-420/G OPF file)
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372 0 obj
<< /S /GoTo /D (subsection.A.2.4) >>
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375 0 obj
(P-420/T OPF file)
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376 0 obj
<< /S /GoTo /D (section.A.3) >>
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379 0 obj
(FCECT)
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380 0 obj
<< /S /GoTo /D (subsection.A.3.1) >>
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(FCECT output spreadsheet parameters)
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<< /S /GoTo /D (subsection.A.3.2) >>
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387 0 obj
(FCECT output file parameters)
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<< /S /GoTo /D (section.A.4) >>
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(ADEBO)
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